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 44324U 26145.45313830 +.00000000 +00000-0 -78202-8 0 00003
2 44324 97.7596 153.2632 0001424 90.5474 269.5909 14.92588302 06
| Epoch (UTC): | 25 May 2026 10:52:31 |
| Eccentricity: | 0.0001424 |
| inclination: | 97.7596° |
| perigee height: | 589 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 153.2632° |
| argument of perigee: | 90.5474° |
| revolutions per day: | 14.92588302 |
| mean anomaly at epoch: | 269.5909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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