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 65907U 26145.07130441 +.00000000 +00000-0 +43803-3 0 00009
2 65907 53.1599 15.4929 0000996 79.2567 280.8548 15.34395790 02
| Epoch (UTC): | 25 May 2026 01:42:40 |
| Eccentricity: | 0.0000996 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 15.4929° |
| argument of perigee: | 79.2567° |
| revolutions per day: | 15.34395790 |
| mean anomaly at epoch: | 280.8548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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