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 00020U 26041.05373832 +.00000000 +00000-0 +42488-3 0 00008
2 00020 33.3451 4.6551 1638306 92.0130 286.8041 11.61813964 05
| Epoch (UTC): | 10 February 2026 01:17:22 |
| Eccentricity: | 0.1638306 |
| inclination: | 33.3451° |
| perigee height: | 507 km |
| apogee height: | 3206 km |
| right ascension of ascending node: | 4.6551° |
| argument of perigee: | 92.0130° |
| revolutions per day: | 11.61813964 |
| mean anomaly at epoch: | 286.8041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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