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 62204U 26145.50003470 +.00000000 +00000-0 +25550-2 0 00003
2 62204 42.9950 186.9046 0018641 67.6797 304.8671 15.51058730 05
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0018641 |
| inclination: | 42.9950° |
| perigee height: | 401 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 186.9046° |
| argument of perigee: | 67.6797° |
| revolutions per day: | 15.51058730 |
| mean anomaly at epoch: | 304.8671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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