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 62242U 26145.66438068 +.00000000 +00000-0 +15664-3 0 00003
2 62242 89.0099 24.7199 0015984 77.9737 282.3204 13.51005841 01
| Epoch (UTC): | 25 May 2026 15:56:42 |
| Eccentricity: | 0.0015984 |
| inclination: | 89.0099° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 24.7199° |
| argument of perigee: | 77.9737° |
| revolutions per day: | 13.51005841 |
| mean anomaly at epoch: | 282.3204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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