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 66899U 26145.39964331 +.00000000 +00000-0 +74130-3 0 00005
2 66899 53.1602 27.5115 0003034 73.6767 286.4569 15.34395650 05
| Epoch (UTC): | 25 May 2026 09:35:29 |
| Eccentricity: | 0.0003034 |
| inclination: | 53.1602° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 27.5115° |
| argument of perigee: | 73.6767° |
| revolutions per day: | 15.34395650 |
| mean anomaly at epoch: | 286.4569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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