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 00022U 26039.13167353 +.00000000 +00000-0 +67925-3 0 00008
2 00022 50.2467 16.9535 0083769 325.2584 34.2922 15.25634191 00
| Epoch (UTC): | 08 February 2026 03:09:36 |
| Eccentricity: | 0.0083769 |
| inclination: | 50.2467° |
| perigee height: | 431 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 16.9535° |
| argument of perigee: | 325.2584° |
| revolutions per day: | 15.25634191 |
| mean anomaly at epoch: | 34.2922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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