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 22980U 26017.67062459 +.00000000 +00000-0 +27642-3 0 00003
2 22980 28.3811 216.2615 6634162 178.0305 187.3551 3.09408385 01
| Epoch (UTC): | 17 January 2026 16:05:41 |
| Eccentricity: | 0.6634162 |
| inclination: | 28.3811° |
| perigee height: | 318 km |
| apogee height: | 26713 km |
| right ascension of ascending node: | 216.2615° |
| argument of perigee: | 178.0305° |
| revolutions per day: | 3.09408385 |
| mean anomaly at epoch: | 187.3551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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