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 64296U 26145.56188649 +.00000000 +00000-0 +34935-3 0 00002
2 64296 70.0011 0.6228 0002771 260.4856 99.5990 14.98344422 06
| Epoch (UTC): | 25 May 2026 13:29:06 |
| Eccentricity: | 0.0002771 |
| inclination: | 70.0011° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.6228° |
| argument of perigee: | 260.4856° |
| revolutions per day: | 14.98344422 |
| mean anomaly at epoch: | 99.5990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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