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 44349U 26145.44246249 +.00000000 +00000-0 +15250-3 0 00006
2 44349 23.9963 185.7208 0000395 265.4255 94.6200 14.96394460 02
| Epoch (UTC): | 25 May 2026 10:37:08 |
| Eccentricity: | 0.0000395 |
| inclination: | 23.9963° |
| perigee height: | 578 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 185.7208° |
| argument of perigee: | 265.4255° |
| revolutions per day: | 14.96394460 |
| mean anomaly at epoch: | 94.6200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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