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 54135U 26145.45746260 +.00000000 +00000-0 +12242-3 0 00007
2 54135 87.9156 309.4953 0002089 90.7469 269.3903 13.19726263 05
| Epoch (UTC): | 25 May 2026 10:58:44 |
| Eccentricity: | 0.0002089 |
| inclination: | 87.9156° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4953° |
| argument of perigee: | 90.7469° |
| revolutions per day: | 13.19726263 |
| mean anomaly at epoch: | 269.3903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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