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 66987U 26145.16264258 +.00000000 +00000-0 +89498-3 0 00002
2 66987 43.0000 311.5078 0001371 273.1548 86.9146 15.27590227 06
| Epoch (UTC): | 25 May 2026 03:54:12 |
| Eccentricity: | 0.0001371 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 311.5078° |
| argument of perigee: | 273.1548° |
| revolutions per day: | 15.27590227 |
| mean anomaly at epoch: | 86.9146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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