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 26145.57036095 +.00000000 +00000-0 +50710-4 0 00009
2 44873 97.8887 329.5006 0001408 94.2251 265.9123 14.82160649 05
| Epoch (UTC): | 25 May 2026 13:41:19 |
| Eccentricity: | 0.0001408 |
| inclination: | 97.8887° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 329.5006° |
| argument of perigee: | 94.2251° |
| revolutions per day: | 14.82160649 |
| mean anomaly at epoch: | 265.9123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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