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 42984U 26145.60615279 +.00000000 +00000-0 +00000-0 0 00004
2 42984 0.0084 315.8992 0000866 101.0065 157.6569 1.00272520 09
| Epoch (UTC): | 25 May 2026 14:32:51 |
| Eccentricity: | 0.0000866 |
| inclination: | 0.0084° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 315.8992° |
| argument of perigee: | 101.0065° |
| revolutions per day: | 1.00272520 |
| mean anomaly at epoch: | 157.6569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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