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 62846U 26145.34297810 +.00000000 +00000-0 +77607-3 0 00001
2 62846 43.0040 16.1191 0001595 273.4615 86.6054 15.27603074 00
| Epoch (UTC): | 25 May 2026 08:13:53 |
| Eccentricity: | 0.0001595 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 16.1191° |
| argument of perigee: | 273.4615° |
| revolutions per day: | 15.27603074 |
| mean anomaly at epoch: | 86.6054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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