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 54372U 26145.34829794 +.00000000 +00000-0 +41275-3 0 00000
2 54372 34.9996 109.1160 0000501 100.9299 259.1476 15.33765873 09
| Epoch (UTC): | 25 May 2026 08:21:32 |
| Eccentricity: | 0.0000501 |
| inclination: | 34.9996° |
| perigee height: | 464 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 109.1160° |
| argument of perigee: | 100.9299° |
| revolutions per day: | 15.33765873 |
| mean anomaly at epoch: | 259.1476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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