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 00202U 26053.81689471 +.00000000 +00000-0 +79652-4 0 00000
2 00202 32.4351 215.1631 0100585 65.8627 295.2476 13.63781286 06
| Epoch (UTC): | 22 February 2026 19:36:19 |
| Eccentricity: | 0.0100585 |
| inclination: | 32.4351° |
| perigee height: | 948 km |
| apogee height: | 1096 km |
| right ascension of ascending node: | 215.1631° |
| argument of perigee: | 65.8627° |
| revolutions per day: | 13.63781286 |
| mean anomaly at epoch: | 295.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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