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 42901U 26088.20240514 +.00000000 +00000-0 +41973-3 0 00008
2 42901 97.2814 128.3330 0001703 285.2806 74.8238 15.13767402 09
| Epoch (UTC): | 29 March 2026 04:51:27 |
| Eccentricity: | 0.0001703 |
| inclination: | 97.2814° |
| perigee height: | 524 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 128.3330° |
| argument of perigee: | 285.2806° |
| revolutions per day: | 15.13767402 |
| mean anomaly at epoch: | 74.8238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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