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 44341U 26145.24591211 +.00000000 +00000-0 +20300-3 0 00000
2 44341 23.9954 125.6470 0011234 112.3889 247.7794 14.57161568 02
| Epoch (UTC): | 25 May 2026 05:54:06 |
| Eccentricity: | 0.0011234 |
| inclination: | 23.9954° |
| perigee height: | 694 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 125.6470° |
| argument of perigee: | 112.3889° |
| revolutions per day: | 14.57161568 |
| mean anomaly at epoch: | 247.7794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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