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 57891U 26145.55970997 +.00000000 +00000-0 +67887-5 0 00003
2 57891 42.9971 239.9920 0001653 273.9140 86.1522 15.27567872 03
| Epoch (UTC): | 25 May 2026 13:25:58 |
| Eccentricity: | 0.0001653 |
| inclination: | 42.9971° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9920° |
| argument of perigee: | 273.9140° |
| revolutions per day: | 15.27567872 |
| mean anomaly at epoch: | 86.1522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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