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 62444U 26145.25726950 +.00000000 +00000-0 +38032-3 0 00006
2 62444 53.1640 337.3505 0001684 83.4675 276.6517 15.30231261 07
| Epoch (UTC): | 25 May 2026 06:10:28 |
| Eccentricity: | 0.0001684 |
| inclination: | 53.1640° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.3505° |
| argument of perigee: | 83.4675° |
| revolutions per day: | 15.30231261 |
| mean anomaly at epoch: | 276.6517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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