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 57762U 26145.37496456 +.00000000 +00000-0 +26793-4 0 00003
2 57762 81.0020 29.3114 0007337 70.8892 289.3059 13.85472510 06
| Epoch (UTC): | 25 May 2026 08:59:56 |
| Eccentricity: | 0.0007337 |
| inclination: | 81.0020° |
| perigee height: | 939 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 29.3114° |
| argument of perigee: | 70.8892° |
| revolutions per day: | 13.85472510 |
| mean anomaly at epoch: | 289.3059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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