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 61916U 26145.58335647 +.00000000 +00000-0 +19434-2 0 00008
2 61916 42.9995 211.2181 0001411 278.9134 268.6952 15.27553998 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001411 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.2181° |
| argument of perigee: | 278.9134° |
| revolutions per day: | 15.27553998 |
| mean anomaly at epoch: | 268.6952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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