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 20625U 26066.08159334 +.00000000 +00000-0 -10331-3 0 00003
2 20625 70.9992 303.3924 0016212 303.1052 56.8514 14.15013323 05
| Epoch (UTC): | 07 March 2026 01:57:29 |
| Eccentricity: | 0.0016212 |
| inclination: | 70.9992° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 303.3924° |
| argument of perigee: | 303.1052° |
| revolutions per day: | 14.15013323 |
| mean anomaly at epoch: | 56.8514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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