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 08366U 26104.19500831 +.00000000 +00000-0 +00000-0 0 00006
2 08366 4.7701 278.2672 0004501 2.7550 226.5226 1.00247028 06
| Epoch (UTC): | 14 April 2026 04:40:48 |
| Eccentricity: | 0.0004501 |
| inclination: | 4.7701° |
| perigee height: | 35775 km |
| apogee height: | 35813 km |
| right ascension of ascending node: | 278.2672° |
| argument of perigee: | 2.7550° |
| revolutions per day: | 1.00247028 |
| mean anomaly at epoch: | 226.5226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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