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 04331U 26099.99454700 +.00000000 +00000-0 +11289-3 0 00002
2 04331 99.0058 275.7086 0057506 167.9507 192.3067 14.34603884 06
| Epoch (UTC): | 09 April 2026 23:52:08 |
| Eccentricity: | 0.0057506 |
| inclination: | 99.0058° |
| perigee height: | 735 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 275.7086° |
| argument of perigee: | 167.9507° |
| revolutions per day: | 14.34603884 |
| mean anomaly at epoch: | 192.3067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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