IMPULSE-2 MIRA, 62673
Orbit data source: Space-Track
IMPULSE-2 MIRA, 62673 is a payload satellite owned by Impulse Space (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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62673 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Impulse Space
Mission
Operational Commercial Technology
Bus & Motor
MIRA, AOCS
Mass
250 kg wet, 200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.575 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 IMPULSE-2 MIRA
1 62673U 25009BS 26262.46874840 .00004250 00000-0 18764-3 0 9999
2 62673 97.4177 334.8825 0003349 160.3224 199.8142 15.22280105150940Epoch: 2026-09-19T11:14Z
TLE epoch observation values (Epoch: 2026-09-19T11:14:59.861Z)
Latitude
-0.00006°
Longitude
167.75624°
Altitude
504.225 km
Speed
7.611 km/s
True Right ascension
22h 19m 31s
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
12:09:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.23 km
Perigee altitude
493.626 km
Semi-major axis
6,874.065 km
Eccentricity
0.00033
Inclination
97.4177°
RAAN
334.8825°
Arg. of periapsis
160.3224°
True anomaly
199.8012°
Mean anomaly
199.8142°
Eccentric anomaly
199.8077°
Mean motion
3.80823 °/min
Orbital period
94.53 mins
BSTAR
0.00018764
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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.IMPULSE-2 MIRA 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 | 2026-09-20 04:43:24.975Z | 153.27° SSE | 2026-09-20 04:47:24.975Z | 41.383° NE | 50.971° | 2026-09-20 04:50:24.975Z | 357.256° N |
| 5 mins | 2026-09-20 17:48:24.975Z | 13.927° NNE | 2026-09-20 17:50:24.975Z | 178.562° S | 77.134° | 2026-09-20 17:53:24.975Z | 191.752° SSW |
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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