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 44358U 26145.46445098 +.00000000 +00000-0 +17615-3 0 00008
2 44358 23.9992 61.5556 0000119 263.6930 96.3557 14.96397795 03
| Epoch (UTC): | 25 May 2026 11:08:48 |
| Eccentricity: | 0.0000119 |
| inclination: | 23.9992° |
| perigee height: | 578 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 61.5556° |
| argument of perigee: | 263.6930° |
| revolutions per day: | 14.96397795 |
| mean anomaly at epoch: | 96.3557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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