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 62520U 26145.50751935 +.00000000 +00000-0 +12625-2 0 00009
2 62520 42.9972 327.3681 0000436 269.7092 90.3726 15.70951783 01
| Epoch (UTC): | 25 May 2026 12:10:49 |
| Eccentricity: | 0.0000436 |
| inclination: | 42.9972° |
| perigee height: | 356 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 327.3681° |
| argument of perigee: | 269.7092° |
| revolutions per day: | 15.70951783 |
| mean anomaly at epoch: | 90.3726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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