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 62172U 26145.51370348 +.00000000 +00000-0 +16058-3 0 00003
2 62172 70.0019 330.7059 0002532 263.3617 96.7253 14.98334269 05
| Epoch (UTC): | 25 May 2026 12:19:43 |
| Eccentricity: | 0.0002532 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.7059° |
| argument of perigee: | 263.3617° |
| revolutions per day: | 14.98334269 |
| mean anomaly at epoch: | 96.7253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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