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 65800U 26145.56752747 +.00000000 +00000-0 +16037-3 0 00003
2 65800 97.4524 8.2823 0001865 88.1089 272.0352 15.05655221 02
| Epoch (UTC): | 25 May 2026 13:37:14 |
| Eccentricity: | 0.0001865 |
| inclination: | 97.4524° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2823° |
| argument of perigee: | 88.1089° |
| revolutions per day: | 15.05655221 |
| mean anomaly at epoch: | 272.0352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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