LEMUR 2 ARIANNA, 62699
Orbit data source: Space-Track
LEMUR 2 ARIANNA, 62699 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 2025 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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62699 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.063 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LEMUR 2 ARIANNA
1 62699U 25009CU 26124.79164612 .00008241 00000-0 63658-3 0 9995
2 62699 97.6825 206.5657 0000500 296.0397 64.0776 15.01789507 71048Epoch: 2026-05-04T18:59Z
TLE epoch observation values (Epoch: 2026-05-04T18:59:58.224Z)
Latitude
-0.00003°
Longitude
58.89734°
Altitude
564.284 km
Speed
7.579 km/s
True Right ascension
13h 46m 15s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:49:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.727 km
Perigee altitude
558.033 km
Semi-major axis
6,936.517 km
Eccentricity
0.00005
Inclination
97.6825°
RAAN
206.5657°
Arg. of periapsis
296.0397°
True anomaly
64.08275°
Mean anomaly
64.0776°
Eccentric anomaly
64.08018°
Mean motion
3.75691 °/min
Orbital period
95.82 mins
BSTAR
0.00063658
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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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.LEMUR 2 ARIANNA 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-05 17:57:02.551Z | 25.366° NE | 2026-05-05 18:01:02.551Z | 122.047° SE | 35.578° | 2026-05-05 18:04:02.551Z | 173.047° S |
| 5 mins | 2026-05-06 04:44:02.551Z | 114.569° SE | 2026-05-06 04:46:02.551Z | 73.321° E | 23.912° | 2026-05-06 04:49:02.551Z | 16.884° NNE |
| 5 mins | 2026-05-06 06:19:02.551Z | 226.283° WSW | 2026-05-06 06:21:02.551Z | 264.447° W | 20.198° | 2026-05-06 06:24:02.551Z | 315.129° NNW |
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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