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 23405U 26071.16978169 +.00000000 +00000-0 +78284-4 0 00003
2 23405 70.9853 347.2721 0002954 208.8129 151.2831 14.15561637 04
| Epoch (UTC): | 12 March 2026 04:04:29 |
| Eccentricity: | 0.0002954 |
| inclination: | 70.9853° |
| perigee height: | 838 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 347.2721° |
| argument of perigee: | 208.8129° |
| revolutions per day: | 14.15561637 |
| mean anomaly at epoch: | 151.2831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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