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 26039.46797926 +.00000000 +00000-0 +99340-4 0 00007
2 22803 70.9892 72.7519 0019495 256.6657 103.2293 14.17227484 08
| Epoch (UTC): | 08 February 2026 11:13:53 |
| Eccentricity: | 0.0019495 |
| inclination: | 70.9892° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 72.7519° |
| argument of perigee: | 256.6657° |
| revolutions per day: | 14.17227484 |
| mean anomaly at epoch: | 103.2293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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