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 44072U 26145.61530145 +.00000000 +00000-0 +76456-4 0 00005
2 44072 97.8642 220.7234 0001406 87.4353 272.7022 14.83650811 05
| Epoch (UTC): | 25 May 2026 14:46:02 |
| Eccentricity: | 0.0001406 |
| inclination: | 97.8642° |
| perigee height: | 617 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 220.7234° |
| argument of perigee: | 87.4353° |
| revolutions per day: | 14.83650811 |
| mean anomaly at epoch: | 272.7022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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