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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 ARIANNA
1 62699U 25009CU 25286.17153997 .00015777 00000-0 13629-2 0 9993
2 62699 97.7257 4.8685 0003408 133.4659 226.6847 14.97306742 40527Epoch: 2025-10-13T04:07Z
TLE epoch observation values (Epoch: 2025-10-13T04:07:01.053Z)
Latitude
0°
Longitude
-78.86403°
Altitude
579.899 km
Speed
7.57 km/s
True Right ascension
00h 19m 28s
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
08:59:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.601 km
Perigee altitude
569.863 km
Semi-major axis
6,950.369 km
Eccentricity
0.00034
Inclination
97.7257°
RAAN
4.8685°
Arg. of periapsis
133.4659°
True anomaly
226.65629°
Mean anomaly
226.6847°
Eccentric anomaly
226.6705°
Mean motion
3.74569 °/min
Orbital period
96.11 mins
BSTAR
0.0013629
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-13 17:31:14.621Z | 38.935° NE | 2025-10-13 17:34:14.621Z | 88.636° E | 23.9° | 2025-10-13 17:37:14.621Z | 147.813° SSE |
| 4 mins | 2025-10-13 19:08:14.621Z | 319.855° NNW | 2025-10-13 19:09:14.621Z | 299.677° NW | 20.612° | 2025-10-13 19:12:14.621Z | 245.07° WSW |
| 5 mins | 2025-10-14 05:55:14.621Z | 210.482° SW | 2025-10-14 05:57:14.621Z | 264.091° W | 30.967° | 2025-10-14 06:00:14.621Z | 325.578° 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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