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 26109.48983036 +.00000000 +00000-0 +29008-3 0 00008
2 00022 50.2458 30.1118 0079415 247.8178 111.4341 15.27701045 04
| Epoch (UTC): | 19 April 2026 11:45:21 |
| Eccentricity: | 0.0079415 |
| inclination: | 50.2458° |
| perigee height: | 428 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 30.1118° |
| argument of perigee: | 247.8178° |
| revolutions per day: | 15.27701045 |
| mean anomaly at epoch: | 111.4341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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