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 22220U 26041.94827757 +.00000000 +00000-0 -49763-5 0 00008
2 22220 70.9978 244.7044 0011395 144.3993 322.8524 14.16856001 05
| Epoch (UTC): | 10 February 2026 22:45:31 |
| Eccentricity: | 0.0011395 |
| inclination: | 70.9978° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 244.7044° |
| argument of perigee: | 144.3993° |
| revolutions per day: | 14.16856001 |
| mean anomaly at epoch: | 322.8524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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