DECAYED

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IM-2, 63099 (Decayed)

Orbit data source: Space-Track

IM-2, 63099 was a payload satellite owned by Intuitive Mach. (US) in HEO that was launched on Thu, 27 Feb 2025 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/63099?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63099, 2025-038A

Orbit

Decayed

Last TLE update

5 months ago

Origin

Intuitive Machines LLC (US)

Manufacturer

Intuitive Mach.

Mission

Decayed Commercial Planetary

Bus & Motor

NOVA-C, AOCS

Mass

2,120 kg wet, ~650 kg dry

Launch date (UTC)

2025-02-27 (5 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 6 Leg, 2.3 m

Radar Cross Section

8.160 m²

Expand to show TLE details & history

TLE from 5 months ago

0 IM-2
1 63099U 25038A   25058.03746186 -.00007054  00000-0  00000-0 0  9997
2 63099  28.5200 357.2438 9653600 216.4100   0.0142  0.10463308    03

Epoch: 2025-02-27T00:53Z

TLE epoch observation values (Epoch: 2025-02-27T00:53:56.704Z)

Latitude

-2.41715°

Longitude

-177.27109°

Altitude

51,153.232 km

Speed

3.429 km/s

True Right ascension

23h 33m 20s

True Declination

-2° 24' 55"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

367,518.128 km

Perigee altitude

211.885 km

Semi-major axis

190,243.144 km

Eccentricity

0.96536

Inclination

28.52°

RAAN

357.2438°

Arg. of periapsis

216.41°

True anomaly

3.0537°

Mean anomaly

0.0142°

Eccentric anomaly

0.4055°

Mean motion

0.02616 °/min

Orbital period

13,763.31 mins

BSTAR

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Other satellites on launch #38 in the year 2025 (2025-02-27 UTC)

CHIMERA-1, 63100

LUNAR TRAILBLAZER, 63101

BROKKER-2 ODIN, 63102

FALCON 9 R/B, 63103

IM-2 Visibility forecast

Observer location: undefined°, undefined°

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.
542 mins	2025-07-19 11:25:38.496Z	106.505° ESE	2025-07-19 14:14:38.496Z	180.552° SSW	43.241°	2025-07-19 20:27:38.496Z	287.42° WNW
174 mins	2025-07-20 08:31:38.496Z	71.959° E	2025-07-20 11:25:38.496Z	97.656° ESE	34.132°	2025-07-20 11:25:38.496Z	97.656° ESE

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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Authenticating...

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Check out IM-2, 63099 (Decayed) on other resources

View IM-2, 63099 (Decayed) on Celestrak

View IM-2, 63099 (Decayed) on Gunter's Space Page

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