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 04589U 26088.20748846 +.00000000 +00000-0 +10310-3 0 00000
2 04589 74.0593 142.1172 0021637 268.0716 91.7963 14.43312307 06
| Epoch (UTC): | 29 March 2026 04:58:47 |
| Eccentricity: | 0.0021637 |
| inclination: | 74.0593° |
| perigee height: | 732 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 142.1172° |
| argument of perigee: | 268.0716° |
| revolutions per day: | 14.43312307 |
| mean anomaly at epoch: | 91.7963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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