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 65100U 26145.39811622 +.00000000 +00000-0 +64675-3 0 00006
2 65100 53.1612 29.6875 0001315 80.9847 279.1305 15.34415678 06
| Epoch (UTC): | 25 May 2026 09:33:17 |
| Eccentricity: | 0.0001315 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.6875° |
| argument of perigee: | 80.9847° |
| revolutions per day: | 15.34415678 |
| mean anomaly at epoch: | 279.1305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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