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 04579U 26074.80163488 +.00000000 +00000-0 +94962-4 0 00009
2 04579 73.9995 94.3477 0009210 30.9419 329.2289 14.63602658 07
| Epoch (UTC): | 15 March 2026 19:14:21 |
| Eccentricity: | 0.0009210 |
| inclination: | 73.9995° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 94.3477° |
| argument of perigee: | 30.9419° |
| revolutions per day: | 14.63602658 |
| mean anomaly at epoch: | 329.2289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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