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SPACEMOBILE-002, 61048

Orbit data source: Space-Track

SPACEMOBILE-002, 61048 is a payload satellite owned by AST & Science (US) in LEO that was launched on Thu, 12 Sep 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe URL

https://www.satcat.com/sats-embedded/61048?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61048, 2024-163D

Orbit

LEO

Country

Related business

AST SpaceMoblie (US)

Manufacturer

AST & Science

Mission

Operational Commercial Communications

Bus & Motor

BW3, Unknown motor

Mass

1,500 kg wet, 1,500 kg dry

Launch date (UTC)

2024-09-12 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Plate, 6.5 m

Radar Cross Section

32.590 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 SPACEMOBILE-002
1 61048U 24163D   26225.69159367  .00009401  00000-0  43848-3 0  9992
2 61048  52.9733  44.7660 0003989 291.9988  68.0582 15.20528778106519

Epoch: 2026-08-13T16:35Z

TLE epoch observation values (Epoch: 2026-08-13T16:35:53.693Z)

Latitude

-0.00001°

Longitude

-166.33526°

Altitude

504.096 km

Speed

7.614 km/s

True Right ascension

02h 59m 03s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

11:55:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

507.275 km

Perigee altitude

501.784 km

Semi-major axis

6,882.667 km

Eccentricity

0.0004

Inclination

52.9733°

RAAN

44.766°

Arg. of periapsis

291.9988°

True anomaly

68.10061°

Mean anomaly

68.0582°

Eccentric anomaly

68.0794°

Mean motion

3.80109 °/min

Orbital period

94.71 mins

BSTAR

0.00043848

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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)

SPACEMOBILE-SSR04 DEB, 62372

SPACEMOBILE-001, 61047

SPACEMOBILE-SSR03 DEB, 62371

SPACEMOBILE-SSR05 DEB, 62373

SPACEMOBILE-003, 61045

SPACEMOBILE-005, 61046

SPACEMOBILE-SSR02 DEB, 62370

SPACEMOBILE-004, 61049

SPACEMOBILE-SSR01 DEB, 62369

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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SPACEMOBILE-002 Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
5 mins	2026-08-17 13:52:47.818Z	245.336° WSW	2026-08-17 13:54:47.818Z	332.574° NNW	42.79°	2026-08-17 13:57:47.818Z	44.397° NE
4 mins	2026-08-17 18:51:47.818Z	348.832° N	2026-08-17 18:53:47.818Z	31.74° NE	20.335°	2026-08-17 18:55:47.818Z	68.471° E
6 mins	2026-08-17 20:29:47.818Z	303.932° NW	2026-08-17 20:32:47.818Z	170.84° S	42.014°	2026-08-17 20:35:47.818Z	138.115° SSE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out SPACEMOBILE-002, 61048 on other resources

View SPACEMOBILE-002, 61048 on NASA - NSSDCA Website

View SPACEMOBILE-002, 61048 on Heavens-Above

View SPACEMOBILE-002, 61048 on Keep Track

View SPACEMOBILE-002, 61048 on Celestrak

View SPACEMOBILE-002, 61048 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

SPACEMOBILE-002, 61048

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-08-13T16:35:53.693Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)

SPACEMOBILE-002 Visibility forecast

Co-orbital & Co-planar RSOs

Check out SPACEMOBILE-002, 61048 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago