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 22803U 26042.07948899 +.00000000 +00000-0 +20435-4 0 00004
2 22803 70.9891 67.2437 0019486 253.2008 106.6978 14.17228169 06
| Epoch (UTC): | 11 February 2026 01:54:27 |
| Eccentricity: | 0.0019486 |
| inclination: | 70.9891° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 67.2437° |
| argument of perigee: | 253.2008° |
| revolutions per day: | 14.17228169 |
| mean anomaly at epoch: | 106.6978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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