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 62334U 26145.63496698 +.00000000 +00000-0 +42884-3 0 00009
2 62334 97.5362 93.9221 0002473 83.4524 276.6989 15.13808783 01
| Epoch (UTC): | 25 May 2026 15:14:21 |
| Eccentricity: | 0.0002473 |
| inclination: | 97.5362° |
| perigee height: | 523 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 93.9221° |
| argument of perigee: | 83.4524° |
| revolutions per day: | 15.13808783 |
| mean anomaly at epoch: | 276.6989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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