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 55639U 26145.27612602 +.00000000 +00000-0 -19537-3 0 00004
2 55639 69.9993 351.3419 0002624 269.5460 90.5398 14.98310623 08
| Epoch (UTC): | 25 May 2026 06:37:37 |
| Eccentricity: | 0.0002624 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.3419° |
| argument of perigee: | 269.5460° |
| revolutions per day: | 14.98310623 |
| mean anomaly at epoch: | 90.5398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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