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 22488U 26103.23763041 +.00000000 +00000-0 +29768-4 0 00001
2 22488 82.9456 200.2840 0025217 191.1588 197.7037 13.77997090 02
| Epoch (UTC): | 13 April 2026 05:42:11 |
| Eccentricity: | 0.0025217 |
| inclination: | 82.9456° |
| perigee height: | 952 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 200.2840° |
| argument of perigee: | 191.1588° |
| revolutions per day: | 13.77997090 |
| mean anomaly at epoch: | 197.7037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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