SPACEBEE-7, 43816
Orbit data source: Space-Track
SPACEBEE-7, 43816 is a payload satellite owned by Swarm Tech (US) in SSO that was launched on Mon, 03 Dec 2018 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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43816 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Swarm Tech
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.017 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SPACEBEE-7
1 43816U 18099BL 25286.24023136 .00085192 00000-0 16892-2 0 9996
2 43816 97.4814 359.4754 0004076 28.4644 331.6827 15.46719627376148Epoch: 2025-10-13T05:45Z
TLE epoch observation values (Epoch: 2025-10-13T05:45:55.989Z)
Latitude
-0.00005°
Longitude
-109.05373°
Altitude
427.012 km
Speed
7.657 km/s
True Right ascension
23h 57m 54s
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
09:31:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
426.036 km
Perigee altitude
420.491 km
Semi-major axis
6,801.401 km
Eccentricity
0.00041
Inclination
97.4814°
RAAN
359.4754°
Arg. of periapsis
28.4644°
True anomaly
331.66053°
Mean anomaly
331.6827°
Eccentric anomaly
331.67162°
Mean motion
3.86942 °/min
Orbital period
93.04 mins
BSTAR
0.0016892
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.SPACEBEE-7 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-13 17:12:25.455Z | 50.062° ENE | 2025-10-13 17:14:25.455Z | 94.817° ESE | 20.152° | 2025-10-13 17:16:25.455Z | 140.816° SSE |
| 5 mins | 2025-10-14 05:11:25.455Z | 179.059° S | 2025-10-14 05:13:25.455Z | 237.433° WSW | 42.032° | 2025-10-14 05:16:25.455Z | 341.217° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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