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 66949U 26145.02858506 +.00000000 +00000-0 +52243-3 0 00008
2 66949 53.1601 3.2183 0000810 61.4243 298.6841 15.34421098 03
| Epoch (UTC): | 25 May 2026 00:41:09 |
| Eccentricity: | 0.0000810 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.2183° |
| argument of perigee: | 61.4243° |
| revolutions per day: | 15.34421098 |
| mean anomaly at epoch: | 298.6841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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