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 54140U 26145.39744588 +.00000000 +00000-0 +16831-3 0 00005
2 54140 87.9160 309.4981 0001747 88.7124 271.4208 13.19726301 07
| Epoch (UTC): | 25 May 2026 09:32:19 |
| Eccentricity: | 0.0001747 |
| inclination: | 87.9160° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4981° |
| argument of perigee: | 88.7124° |
| revolutions per day: | 13.19726301 |
| mean anomaly at epoch: | 271.4208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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