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 26088.20813652 +.00000000 +00000-0 +14697-3 0 00009
2 20625 70.9977 256.9174 0016352 274.0604 85.8650 14.15016510 06
| Epoch (UTC): | 29 March 2026 04:59:42 |
| Eccentricity: | 0.0016352 |
| inclination: | 70.9977° |
| perigee height: | 830 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 256.9174° |
| argument of perigee: | 274.0604° |
| revolutions per day: | 14.15016510 |
| mean anomaly at epoch: | 85.8650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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