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 62101U 26145.45025588 +.00000000 +00000-0 +54485-3 0 00007
2 62101 42.9991 131.7902 0001444 276.3426 83.7261 15.27592649 09
| Epoch (UTC): | 25 May 2026 10:48:22 |
| Eccentricity: | 0.0001444 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.7902° |
| argument of perigee: | 276.3426° |
| revolutions per day: | 15.27592649 |
| mean anomaly at epoch: | 83.7261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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