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, 1.2 m
Radar Cross Section
0.575 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 IMPULSE-2 MIRA
1 62673U 25009BS 26171.47801973 .00007402 00000-0 30012-3 0 9998
2 62673 97.3865 245.3959 0003272 151.5628 208.5789 15.24922962137094Epoch: 2026-06-20T11:28Z
TLE epoch observation values (Epoch: 2026-06-20T11:28:20.904Z)
Latitude
-0.00003°
Longitude
164.61673°
Altitude
496.089 km
Speed
7.616 km/s
True Right ascension
16h 21m 35s
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
07:21:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.222 km
Perigee altitude
485.729 km
Semi-major axis
6,866.112 km
Eccentricity
0.00033
Inclination
97.3865°
RAAN
245.3959°
Arg. of periapsis
151.5628°
True anomaly
208.56097°
Mean anomaly
208.5789°
Eccentric anomaly
208.56993°
Mean motion
3.81484 °/min
Orbital period
94.37 mins
BSTAR
0.00030012
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 04:55:32.303Z | 162.434° S | 2026-06-21 04:58:32.303Z | 34.264° NE | 44.087° | 2026-06-21 05:01:32.303Z | 351° N |
| 5 mins | 2026-06-21 17:58:32.303Z | 0.224° NNE | 2026-06-21 18:00:32.303Z | 244.442° WSW | 41.96° | 2026-06-21 18:03:32.303Z | 200.91° 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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