View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53081U 26145.47318986 +.00000000 +00000-0 +51519-3 0 00008
2 53081 97.4479 325.3689 0001439 101.8009 258.3380 15.05616475 00
| Epoch (UTC): | 25 May 2026 11:21:23 |
| Eccentricity: | 0.0001439 |
| inclination: | 97.4479° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.3689° |
| argument of perigee: | 101.8009° |
| revolutions per day: | 15.05616475 |
| mean anomaly at epoch: | 258.3380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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