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 54134U 26145.02309841 +.00000000 +00000-0 +21564-4 0 00007
2 54134 87.9148 309.5910 0001652 93.8026 266.3296 13.19726706 01
| Epoch (UTC): | 25 May 2026 00:33:15 |
| Eccentricity: | 0.0001652 |
| inclination: | 87.9148° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5910° |
| argument of perigee: | 93.8026° |
| revolutions per day: | 13.19726706 |
| mean anomaly at epoch: | 266.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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