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 21610U 26156.39942958 +.00000000 +00000-0 +10569-3 0 00006
2 21610 98.1880 205.2747 0003700 147.6026 212.5392 14.42949895 08
| Epoch (UTC): | 05 June 2026 09:35:10 |
| Eccentricity: | 0.0003700 |
| inclination: | 98.1880° |
| perigee height: | 746 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 205.2747° |
| argument of perigee: | 147.6026° |
| revolutions per day: | 14.42949895 |
| mean anomaly at epoch: | 212.5392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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