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 62082U 26145.59606683 +.00000000 +00000-0 +13224-3 0 00007
2 62082 97.9131 305.0657 0004669 3.1271 356.9965 14.72398014 07
| Epoch (UTC): | 25 May 2026 14:18:20 |
| Eccentricity: | 0.0004669 |
| inclination: | 97.9131° |
| perigee height: | 650 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 305.0657° |
| argument of perigee: | 3.1271° |
| revolutions per day: | 14.72398014 |
| mean anomaly at epoch: | 356.9965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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