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 62825U 26145.49207947 +.00000000 +00000-0 +72645-3 0 00003
2 62825 53.1586 310.2646 0000946 106.7916 253.3189 15.30196660 02
| Epoch (UTC): | 25 May 2026 11:48:35 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.2646° |
| argument of perigee: | 106.7916° |
| revolutions per day: | 15.30196660 |
| mean anomaly at epoch: | 253.3189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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