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 66183U 26145.00003001 +.00000000 +00000-0 +81201-3 0 00004
2 66183 53.1577 251.0548 0001212 88.0818 272.0321 15.30201701 05
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 251.0548° |
| argument of perigee: | 88.0818° |
| revolutions per day: | 15.30201701 |
| mean anomaly at epoch: | 272.0321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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