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 67542U 26145.26356372 +.00000000 +00000-0 +49340-3 0 00002
2 67542 97.2858 32.3866 0002290 82.1592 277.9911 15.33446321 01
| Epoch (UTC): | 25 May 2026 06:19:31 |
| Eccentricity: | 0.0002290 |
| inclination: | 97.2858° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.3866° |
| argument of perigee: | 82.1592° |
| revolutions per day: | 15.33446321 |
| mean anomaly at epoch: | 277.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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