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 02091U 26088.20746550 +.00000000 +00000-0 +74745-6 0 00001
2 02091 101.2374 359.4141 0039237 59.0485 97.0786 12.69429456 09
| Epoch (UTC): | 29 March 2026 04:58:45 |
| Eccentricity: | 0.0039237 |
| inclination: | 101.2374° |
| perigee height: | 1354 km |
| apogee height: | 1415 km |
| right ascension of ascending node: | 359.4141° |
| argument of perigee: | 59.0485° |
| revolutions per day: | 12.69429456 |
| mean anomaly at epoch: | 97.0786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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