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 62069U 26145.18347488 +.00000000 +00000-0 +88728-3 0 00003
2 62069 53.1574 54.4692 0000805 106.3320 253.7786 15.69755443 05
| Epoch (UTC): | 25 May 2026 04:24:12 |
| Eccentricity: | 0.0000805 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.4692° |
| argument of perigee: | 106.3320° |
| revolutions per day: | 15.69755443 |
| mean anomaly at epoch: | 253.7786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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