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 57360U 26145.52260144 +.00000000 +00000-0 +37374-4 0 00004
2 57360 43.0031 167.4495 0001721 268.6189 91.4466 15.27577606 07
| Epoch (UTC): | 25 May 2026 12:32:32 |
| Eccentricity: | 0.0001721 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.4495° |
| argument of perigee: | 268.6189° |
| revolutions per day: | 15.27577606 |
| mean anomaly at epoch: | 91.4466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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