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 62448U 26145.51282282 +.00000000 +00000-0 +54289-3 0 00006
2 62448 53.1593 338.7984 0001629 90.4028 269.7160 15.30205252 01
| Epoch (UTC): | 25 May 2026 12:18:27 |
| Eccentricity: | 0.0001629 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.7984° |
| argument of perigee: | 90.4028° |
| revolutions per day: | 15.30205252 |
| mean anomaly at epoch: | 269.7160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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