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 61921U 26145.58046949 +.00000000 +00000-0 +86297-3 0 00000
2 61921 43.0011 207.3205 0001984 272.1107 87.9518 15.27591717 04
| Epoch (UTC): | 25 May 2026 13:55:52 |
| Eccentricity: | 0.0001984 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.3205° |
| argument of perigee: | 272.1107° |
| revolutions per day: | 15.27591717 |
| mean anomaly at epoch: | 87.9518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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