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 54117U 26145.46458470 +.00000000 +00000-0 +33790-3 0 00002
2 54117 87.9150 309.5023 0001759 85.3747 274.7586 13.19725498 06
| Epoch (UTC): | 25 May 2026 11:09:00 |
| Eccentricity: | 0.0001759 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5023° |
| argument of perigee: | 85.3747° |
| revolutions per day: | 13.19725498 |
| mean anomaly at epoch: | 274.7586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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