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 66846U 26145.33417684 +.00000000 +00000-0 +28221-3 0 00005
2 66846 70.0008 141.3248 0003778 267.5099 92.5628 14.98337824 04
| Epoch (UTC): | 25 May 2026 08:01:12 |
| Eccentricity: | 0.0003778 |
| inclination: | 70.0008° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 141.3248° |
| argument of perigee: | 267.5099° |
| revolutions per day: | 14.98337824 |
| mean anomaly at epoch: | 92.5628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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