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 57757U 26145.12100589 +.00000000 +00000-0 +16604-3 0 00008
2 57757 81.0131 23.9402 0008042 52.3560 307.8348 14.28611931 01
| Epoch (UTC): | 25 May 2026 02:54:14 |
| Eccentricity: | 0.0008042 |
| inclination: | 81.0131° |
| perigee height: | 791 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 23.9402° |
| argument of perigee: | 52.3560° |
| revolutions per day: | 14.28611931 |
| mean anomaly at epoch: | 307.8348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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