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 54116U 26145.40534299 +.00000000 +00000-0 +13249-3 0 00006
2 54116 87.9154 309.5038 0001749 92.3197 267.8136 13.19726439 01
| Epoch (UTC): | 25 May 2026 09:43:41 |
| Eccentricity: | 0.0001749 |
| inclination: | 87.9154° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5038° |
| argument of perigee: | 92.3197° |
| revolutions per day: | 13.19726439 |
| mean anomaly at epoch: | 267.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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