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 62394U 26145.37969828 +.00000000 +00000-0 +70668-3 0 00007
2 62394 44.9733 27.9144 0006454 207.7136 152.3410 15.46420907 02
| Epoch (UTC): | 25 May 2026 09:06:45 |
| Eccentricity: | 0.0006454 |
| inclination: | 44.9733° |
| perigee height: | 423 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 27.9144° |
| argument of perigee: | 207.7136° |
| revolutions per day: | 15.46420907 |
| mean anomaly at epoch: | 152.3410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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