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 34813U 26068.84045054 +.00000000 +00000-0 +53059-2 0 00008
2 34813 73.9340 353.0437 0436226 10.5078 350.4785 13.50938738 05
| Epoch (UTC): | 09 March 2026 20:10:14 |
| Eccentricity: | 0.0436226 |
| inclination: | 73.9340° |
| perigee height: | 744 km |
| apogee height: | 1394 km |
| right ascension of ascending node: | 353.0437° |
| argument of perigee: | 10.5078° |
| revolutions per day: | 13.50938738 |
| mean anomaly at epoch: | 350.4785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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