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 54088U 26145.27029003 +.00000000 +00000-0 +24930-3 0 00000
2 54088 53.2140 350.4398 0001580 92.3876 267.7297 15.08816209 03
| Epoch (UTC): | 25 May 2026 06:29:13 |
| Eccentricity: | 0.0001580 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 350.4398° |
| argument of perigee: | 92.3876° |
| revolutions per day: | 15.08816209 |
| mean anomaly at epoch: | 267.7297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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