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 22490U 26145.66573721 +.00000000 +00000-0 +54771-4 0 00003
2 22490 24.9712 346.6311 0041729 259.6357 153.5620 14.46109093 07
| Epoch (UTC): | 25 May 2026 15:58:39 |
| Eccentricity: | 0.0041729 |
| inclination: | 24.9712° |
| perigee height: | 709 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 346.6311° |
| argument of perigee: | 259.6357° |
| revolutions per day: | 14.46109093 |
| mean anomaly at epoch: | 153.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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