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 26083.97987168 +.00000000 +00000-0 +35186-4 0 00008
2 00202 32.4381 64.0784 0101040 295.0729 63.9434 13.63784211 01
| Epoch (UTC): | 24 March 2026 23:31:00 |
| Eccentricity: | 0.0101040 |
| inclination: | 32.4381° |
| perigee height: | 947 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 64.0784° |
| argument of perigee: | 295.0729° |
| revolutions per day: | 13.63784211 |
| mean anomaly at epoch: | 63.9434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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