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 26042.07039771 +.00000000 +00000-0 +69864-4 0 00004
2 08459 74.0590 67.8823 0015322 170.6740 189.4702 14.38190113 07
| Epoch (UTC): | 11 February 2026 01:41:22 |
| Eccentricity: | 0.0015322 |
| inclination: | 74.0590° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 67.8823° |
| argument of perigee: | 170.6740° |
| revolutions per day: | 14.38190113 |
| mean anomaly at epoch: | 189.4702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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