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 62402U 26145.05512418 +.00000000 +00000-0 +74179-3 0 00002
2 62402 44.9726 15.4612 0007106 188.4739 171.6034 15.53268494 00
| Epoch (UTC): | 25 May 2026 01:19:22 |
| Eccentricity: | 0.0007106 |
| inclination: | 44.9726° |
| perigee height: | 402 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 15.4612° |
| argument of perigee: | 188.4739° |
| revolutions per day: | 15.53268494 |
| mean anomaly at epoch: | 171.6034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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