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 63031U 26145.58335647 +.00000000 +00000-0 -11107-3 0 00009
2 63031 53.1602 260.6360 0001415 86.8173 292.0704 15.34384059 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001415 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 260.6360° |
| argument of perigee: | 86.8173° |
| revolutions per day: | 15.34384059 |
| mean anomaly at epoch: | 292.0704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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