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 26075.88793671 +.00000000 +00000-0 +11803-3 0 00003
2 22803 70.9930 355.9478 0018115 205.9642 154.0575 14.17232316 07
| Epoch (UTC): | 16 March 2026 21:18:37 |
| Eccentricity: | 0.0018115 |
| inclination: | 70.9930° |
| perigee height: | 822 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 355.9478° |
| argument of perigee: | 205.9642° |
| revolutions per day: | 14.17232316 |
| mean anomaly at epoch: | 154.0575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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