LEMUR-2 PEGGY-2004, 68479
Orbit data source: Space-Track
LEMUR-2 PEGGY-2004, 68479 is a payload satellite owned by Spire (LU) in SSO that was launched on Mon, 30 Mar 2026 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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68479 intel report (Beta)
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Identifier
Orbit
Country
LU / LUXERelated business
Manufacturer
Spire/Glasgow
Mission
Operational spacecraft
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
Unknown shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 LEMUR-2 PEGGY-2004
1 68479U 26067BR 26171.43689120 .00005525 00000-0 53982-3 0 9992
2 68479 97.7550 129.6668 0001007 116.9085 243.2237 14.92771517 12218Epoch: 2026-06-20T10:29Z
TLE epoch observation values (Epoch: 2026-06-20T10:29:07.399Z)
Latitude
-0.00007°
Longitude
63.73445°
Altitude
592.658 km
Speed
7.563 km/s
True Right ascension
08h 38m 40s
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
10:53:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.017 km
Perigee altitude
585.614 km
Semi-major axis
6,964.453 km
Eccentricity
0.0001
Inclination
97.755°
RAAN
129.6668°
Arg. of periapsis
116.9085°
True anomaly
243.2134°
Mean anomaly
243.2237°
Eccentric anomaly
243.21855°
Mean motion
3.73433 °/min
Orbital period
96.4 mins
BSTAR
0.00053982
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 PEGGY-2004 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 | 2026-06-22 09:42:42.911Z | 29.279° NE | 2026-06-22 09:45:42.911Z | 87.864° E | 34.903° | 2026-06-22 09:49:42.911Z | 171.63° S |
| 5 mins | 2026-06-22 20:33:42.911Z | 108.342° ESE | 2026-06-22 20:35:42.911Z | 61.348° ENE | 25.052° | 2026-06-22 20:38:42.911Z | 12.597° NNE |
| 5 mins | 2026-06-22 22:08:42.911Z | 225.736° WSW | 2026-06-22 22:10:42.911Z | 261.925° W | 20.324° | 2026-06-22 22:13:42.911Z | 312.968° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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