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 54667U 26145.52323050 +.00000000 +00000-0 +12049-3 0 00008
2 54667 87.9260 248.4656 0002038 97.3238 262.8127 13.21825129 04
| Epoch (UTC): | 25 May 2026 12:33:27 |
| Eccentricity: | 0.0002038 |
| inclination: | 87.9260° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4656° |
| argument of perigee: | 97.3238° |
| revolutions per day: | 13.21825129 |
| mean anomaly at epoch: | 262.8127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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