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 43215U 26107.63991405 +.00000000 +00000-0 +62208-5 0 00004
2 43215 97.4446 115.8836 0001707 91.6370 268.5060 15.19145551 08
| Epoch (UTC): | 17 April 2026 15:21:28 |
| Eccentricity: | 0.0001707 |
| inclination: | 97.4446° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 115.8836° |
| argument of perigee: | 91.6370° |
| revolutions per day: | 15.19145551 |
| mean anomaly at epoch: | 268.5060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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