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 26106.89565677 +.00000000 +00000-0 +46201-4 0 00002
2 00202 32.4382 309.3010 0100512 109.3714 251.7803 13.63787417 01
| Epoch (UTC): | 16 April 2026 21:29:44 |
| Eccentricity: | 0.0100512 |
| inclination: | 32.4382° |
| perigee height: | 948 km |
| apogee height: | 1096 km |
| right ascension of ascending node: | 309.3010° |
| argument of perigee: | 109.3714° |
| revolutions per day: | 13.63787417 |
| mean anomaly at epoch: | 251.7803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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