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 44879U 26145.60606000 +.00000000 +00000-0 +35574-3 0 00008
2 44879 97.7805 229.6129 0012458 124.4304 235.8096 14.95309845 00
| Epoch (UTC): | 25 May 2026 14:32:43 |
| Eccentricity: | 0.0012458 |
| inclination: | 97.7805° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 229.6129° |
| argument of perigee: | 124.4304° |
| revolutions per day: | 14.95309845 |
| mean anomaly at epoch: | 235.8096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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