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 66994U 26145.57711807 +.00000000 +00000-0 +27523-3 0 00003
2 66994 97.6322 221.5590 0016203 79.1157 281.1893 15.06286133 08
| Epoch (UTC): | 25 May 2026 13:51:03 |
| Eccentricity: | 0.0016203 |
| inclination: | 97.6322° |
| perigee height: | 536 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 221.5590° |
| argument of perigee: | 79.1157° |
| revolutions per day: | 15.06286133 |
| mean anomaly at epoch: | 281.1893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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