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 61223U 26145.53722446 +.00000000 +00000-0 +27432-3 0 00009
2 61223 98.0414 235.7710 0002934 138.4404 221.7027 14.72314060 08
| Epoch (UTC): | 25 May 2026 12:53:36 |
| Eccentricity: | 0.0002934 |
| inclination: | 98.0414° |
| perigee height: | 652 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 235.7710° |
| argument of perigee: | 138.4404° |
| revolutions per day: | 14.72314060 |
| mean anomaly at epoch: | 221.7027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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