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 65015U 26145.41676654 +.00000000 +00000-0 +68241-3 0 00001
2 65015 53.1604 298.0633 0001913 91.7604 268.3616 15.30212996 00
| Epoch (UTC): | 25 May 2026 10:00:08 |
| Eccentricity: | 0.0001913 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0633° |
| argument of perigee: | 91.7604° |
| revolutions per day: | 15.30212996 |
| mean anomaly at epoch: | 268.3616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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