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 62852U 26145.30434309 +.00000000 +00000-0 +00000-0 0 00000
2 62852 0.0108 302.3861 0000260 49.4965 29.5666 1.00273316 09
| Epoch (UTC): | 25 May 2026 07:18:15 |
| Eccentricity: | 0.0000260 |
| inclination: | 0.0108° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 302.3861° |
| argument of perigee: | 49.4965° |
| revolutions per day: | 1.00273316 |
| mean anomaly at epoch: | 29.5666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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