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 66294U 26145.58671110 +.00000000 +00000-0 +14876-3 0 00006
2 66294 45.3987 242.6934 0004223 296.1849 63.8603 15.20755402 02
| Epoch (UTC): | 25 May 2026 14:04:51 |
| Eccentricity: | 0.0004223 |
| inclination: | 45.3987° |
| perigee height: | 501 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 242.6934° |
| argument of perigee: | 296.1849° |
| revolutions per day: | 15.20755402 |
| mean anomaly at epoch: | 63.8603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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