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 44339U 26145.56044428 +.00000000 +00000-0 +12883-2 0 00001
2 44339 23.9950 265.3322 0006519 125.4682 234.6426 14.89995350 05
| Epoch (UTC): | 25 May 2026 13:27:02 |
| Eccentricity: | 0.0006519 |
| inclination: | 23.9950° |
| perigee height: | 593 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 265.3322° |
| argument of perigee: | 125.4682° |
| revolutions per day: | 14.89995350 |
| mean anomaly at epoch: | 234.6426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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