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 44748U 26145.38838583 +.00000000 +00000-0 +54397-3 0 00005
2 44748 53.0486 182.8583 0001040 70.7916 289.3209 15.61364854 01
| Epoch (UTC): | 25 May 2026 09:19:16 |
| Eccentricity: | 0.0001040 |
| inclination: | 53.0486° |
| perigee height: | 383 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 182.8583° |
| argument of perigee: | 70.7916° |
| revolutions per day: | 15.61364854 |
| mean anomaly at epoch: | 289.3209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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