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 66015U 26145.58335647 +.00000000 +00000-0 +14334-2 0 00007
2 66015 53.1599 106.8766 0003433 36.6674 64.0237 15.34198553 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003433 |
| inclination: | 53.1599° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 106.8766° |
| argument of perigee: | 36.6674° |
| revolutions per day: | 15.34198553 |
| mean anomaly at epoch: | 64.0237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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