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 00801U 26088.22161559 +.00000000 +00000-0 +25992-3 0 00007
2 00801 90.4586 183.8595 0045066 282.4762 77.1387 14.17015515 07
| Epoch (UTC): | 29 March 2026 05:19:07 |
| Eccentricity: | 0.0045066 |
| inclination: | 90.4586° |
| perigee height: | 803 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 183.8595° |
| argument of perigee: | 282.4762° |
| revolutions per day: | 14.17015515 |
| mean anomaly at epoch: | 77.1387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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