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 62199U 26145.47511674 +.00000000 +00000-0 +72090-3 0 00004
2 62199 43.0009 190.1946 0001599 277.8710 82.1960 15.27598585 02
| Epoch (UTC): | 25 May 2026 11:24:10 |
| Eccentricity: | 0.0001599 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 190.1946° |
| argument of perigee: | 277.8710° |
| revolutions per day: | 15.27598585 |
| mean anomaly at epoch: | 82.1960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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