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 66977U 26145.18320402 +.00000000 +00000-0 +58680-3 0 00006
2 66977 43.0009 311.6721 0002244 271.1978 88.8617 15.27589218 07
| Epoch (UTC): | 25 May 2026 04:23:48 |
| Eccentricity: | 0.0002244 |
| inclination: | 43.0009° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 311.6721° |
| argument of perigee: | 271.1978° |
| revolutions per day: | 15.27589218 |
| mean anomaly at epoch: | 88.8617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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