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LEMUR 2 ROCINANTE, 59147

Orbit data source: Space-Track

LEMUR 2 ROCINANTE, 59147 is an American payload satellite in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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/59147?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59147, 2024-043BB

Orbit

SSO

Country

US

Related business

Spire Global (US)

Manufacturer

Spire/Glasgow

Mission

Operational Commercial Communications

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

22 kg wet, 22 kg dry

Launch date (UTC)

2024-03-04 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 4 Pan, 1.4 m

Radar Cross Section

0.326 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 LEMUR 2 ROCINANTE
1 59147U 24043BB  25336.14020634  .00178460  00000-0  17575-2 0  9991
2 59147  97.5101 115.1035 0004053 237.5102 122.5766 15.65393417 97570

Epoch: 2025-12-02T03:21Z

TLE epoch observation values (Epoch: 2025-12-02T03:21:53.827Z)

Latitude

-0.00003°

Longitude

-6.60041°

Altitude

376.73 km

Speed

7.683 km/s

True Right ascension

07h 40m 24s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

11:10:59

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

371.752 km

Perigee altitude

366.283 km

Semi-major axis

6,747.155 km

Eccentricity

0.00041

Inclination

97.5101°

RAAN

115.1035°

Arg. of periapsis

237.5102°

True anomaly

122.61573°

Mean anomaly

122.5766°

Eccentric anomaly

122.59616°

Mean motion

3.91618 °/min

Orbital period

91.93 mins

BSTAR

0.0017575

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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)

JACKAL-01, 59127

PE2_FLT2 (TYVAK-0262), 59104

LACE-1, 59118 (Decayed)

MH-1, 59145 (Decayed)

OBJECT M, 59109 (Decayed)

CONTECSAT-1, 59117

OBJECT AT, 59139 (Decayed)

OBJECT AX, 59143 (Decayed)

JACKAL-02, 59134

OBJECT AW, 59142

Did you know?

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

Click here to try in Sandbox

LEMUR 2 ROCINANTE 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	2025-12-02 22:19:53.653Z	11.517° NNE	2025-12-02 22:21:53.653Z	4.526° NNE	44.064°	2025-12-02 22:24:53.653Z	193.65° SSW

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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 LEMUR 2 ROCINANTE, 59147 on other resources

View LEMUR 2 ROCINANTE, 59147 on NASA - NSSDCA Website

View LEMUR 2 ROCINANTE, 59147 on Heavens-Above

View LEMUR 2 ROCINANTE, 59147 on Keep Track

View LEMUR 2 ROCINANTE, 59147 on Celestrak

View LEMUR 2 ROCINANTE, 59147 on Gunter's Space Page

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

Documentation

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