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 65215U 26145.46842367 +.00000000 +00000-0 +40312-3 0 00003
2 65215 53.1572 157.6585 0000790 74.1561 285.9528 15.34403111 03
| Epoch (UTC): | 25 May 2026 11:14:31 |
| Eccentricity: | 0.0000790 |
| inclination: | 53.1572° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 157.6585° |
| argument of perigee: | 74.1561° |
| revolutions per day: | 15.34403111 |
| mean anomaly at epoch: | 285.9528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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