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 41772U 26145.08154424 +.00000000 +00000-0 +21081-3 0 00005
2 41772 97.0490 186.7567 0003706 46.5945 313.5607 15.34086426 05
| Epoch (UTC): | 25 May 2026 01:57:25 |
| Eccentricity: | 0.0003706 |
| inclination: | 97.0490° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 186.7567° |
| argument of perigee: | 46.5945° |
| revolutions per day: | 15.34086426 |
| mean anomaly at epoch: | 313.5607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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