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 26073.50293456 +.00000000 +00000-0 +12122-3 0 00001
2 04579 73.9996 96.8456 0009155 34.0173 326.1579 14.63601901 00
| Epoch (UTC): | 14 March 2026 12:04:13 |
| Eccentricity: | 0.0009155 |
| inclination: | 73.9996° |
| perigee height: | 675 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 96.8456° |
| argument of perigee: | 34.0173° |
| revolutions per day: | 14.63601901 |
| mean anomaly at epoch: | 326.1579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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