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 08800U 26073.26265716 +.00000000 +00000-0 +32164-4 0 00002
2 08800 81.2542 351.0560 0094136 145.2308 215.5066 14.10651556 05
| Epoch (UTC): | 14 March 2026 06:18:13 |
| Eccentricity: | 0.0094136 |
| inclination: | 81.2542° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 351.0560° |
| argument of perigee: | 145.2308° |
| revolutions per day: | 14.10651556 |
| mean anomaly at epoch: | 215.5066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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