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 26040.52669955 +.00000000 +00000-0 +68763-4 0 00001
2 22803 70.9892 70.5189 0019491 255.2353 104.6611 14.17227876 05
| Epoch (UTC): | 09 February 2026 12:38:26 |
| Eccentricity: | 0.0019491 |
| inclination: | 70.9892° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 70.5189° |
| argument of perigee: | 255.2353° |
| revolutions per day: | 14.17227876 |
| mean anomaly at epoch: | 104.6611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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