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 54129U 26145.19211110 +.00000000 +00000-0 +62020-4 0 00002
2 54129 87.9157 309.5507 0002019 86.8034 273.3330 13.19724411 04
| Epoch (UTC): | 25 May 2026 04:36:38 |
| Eccentricity: | 0.0002019 |
| inclination: | 87.9157° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5507° |
| argument of perigee: | 86.8034° |
| revolutions per day: | 13.19724411 |
| mean anomaly at epoch: | 273.3330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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