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 26088.18447317 +.00000000 +00000-0 +21472-4 0 00008
2 04363 99.8907 3.1222 0001873 170.1915 353.3111 13.46695878 07
| Epoch (UTC): | 29 March 2026 04:25:38 |
| Eccentricity: | 0.0001873 |
| inclination: | 99.8907° |
| perigee height: | 1083 km |
| apogee height: | 1086 km |
| right ascension of ascending node: | 3.1222° |
| argument of perigee: | 170.1915° |
| revolutions per day: | 13.46695878 |
| mean anomaly at epoch: | 353.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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