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 44873U 26088.18639416 +.00000000 +00000-0 +94584-4 0 00005
2 44873 97.8880 272.9434 0001361 85.7352 274.4017 14.82156768 03
| Epoch (UTC): | 29 March 2026 04:28:24 |
| Eccentricity: | 0.0001361 |
| inclination: | 97.8880° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 272.9434° |
| argument of perigee: | 85.7352° |
| revolutions per day: | 14.82156768 |
| mean anomaly at epoch: | 274.4017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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