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 62755U 26145.58335647 +.00000000 +00000-0 -31925-3 0 00001
2 62755 42.9994 80.2929 0001129 262.0986 160.3665 15.27583622 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001129 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 80.2929° |
| argument of perigee: | 262.0986° |
| revolutions per day: | 15.27583622 |
| mean anomaly at epoch: | 160.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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