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 66133U 26145.11631395 +.00000000 +00000-0 +79104-3 0 00003
2 66133 53.1606 44.4944 0001129 80.8554 279.2575 15.30206926 05
| Epoch (UTC): | 25 May 2026 02:47:29 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.4944° |
| argument of perigee: | 80.8554° |
| revolutions per day: | 15.30206926 |
| mean anomaly at epoch: | 279.2575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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