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 57693U 26087.92350977 +.00000000 +00000-0 +64822-3 0 00003
2 57693 53.0075 172.1364 0001497 163.2700 196.8327 14.81103909 08
| Epoch (UTC): | 28 March 2026 22:09:51 |
| Eccentricity: | 0.0001497 |
| inclination: | 53.0075° |
| perigee height: | 625 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 172.1364° |
| argument of perigee: | 163.2700° |
| revolutions per day: | 14.81103909 |
| mean anomaly at epoch: | 196.8327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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