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 04363U 26133.20513875 +.00000000 +00000-0 -13257-5 0 00009
2 04363 99.8899 47.5416 0002736 83.1936 75.0628 13.46697974 09
| Epoch (UTC): | 13 May 2026 04:55:23 |
| Eccentricity: | 0.0002736 |
| inclination: | 99.8899° |
| perigee height: | 1082 km |
| apogee height: | 1086 km |
| right ascension of ascending node: | 47.5416° |
| argument of perigee: | 83.1936° |
| revolutions per day: | 13.46697974 |
| mean anomaly at epoch: | 75.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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