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 62044U 26145.58402294 +.00000000 +00000-0 +52558-3 0 00009
2 62044 43.0023 189.1623 0002225 282.1246 77.9357 15.27591147 06
| Epoch (UTC): | 25 May 2026 14:00:59 |
| Eccentricity: | 0.0002225 |
| inclination: | 43.0023° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 189.1623° |
| argument of perigee: | 282.1246° |
| revolutions per day: | 15.27591147 |
| mean anomaly at epoch: | 77.9357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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