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 08459U 26106.55169683 +.00000000 +00000-0 +30426-4 0 00006
2 08459 74.0600 309.2647 0015080 27.9888 332.2074 14.38223416 07
| Epoch (UTC): | 16 April 2026 13:14:26 |
| Eccentricity: | 0.0015080 |
| inclination: | 74.0600° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 309.2647° |
| argument of perigee: | 27.9888° |
| revolutions per day: | 14.38223416 |
| mean anomaly at epoch: | 332.2074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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