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 43022U 26145.57032738 +.00000000 +00000-0 +30373-3 0 00006
2 43022 97.4832 254.5940 0002532 272.0099 88.0858 15.41781363 02
| Epoch (UTC): | 25 May 2026 13:41:16 |
| Eccentricity: | 0.0002532 |
| inclination: | 97.4832° |
| perigee height: | 439 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 254.5940° |
| argument of perigee: | 272.0099° |
| revolutions per day: | 15.41781363 |
| mean anomaly at epoch: | 88.0858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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