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 20401U 26159.57208549 +.00000000 +00000-0 +00000-0 0 00003
2 20401 12.5031 349.6964 0013632 316.2064 230.4824 0.98995725 06
| Epoch (UTC): | 08 June 2026 13:43:48 |
| Eccentricity: | 0.0013632 |
| inclination: | 12.5031° |
| perigee height: | 36090 km |
| apogee height: | 36206 km |
| right ascension of ascending node: | 349.6964° |
| argument of perigee: | 316.2064° |
| revolutions per day: | 0.98995725 |
| mean anomaly at epoch: | 230.4824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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