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 26106.55825582 +.00000000 +00000-0 +00000-0 0 00001
2 08366 4.7640 278.2386 0004410 2.7441 359.4532 1.00247669 05
| Epoch (UTC): | 16 April 2026 13:23:53 |
| Eccentricity: | 0.0004410 |
| inclination: | 4.7640° |
| perigee height: | 35775 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 278.2386° |
| argument of perigee: | 2.7441° |
| revolutions per day: | 1.00247669 |
| mean anomaly at epoch: | 359.4532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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