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 54099U 26145.54989778 +.00000000 +00000-0 +41200-4 0 00006
2 54099 53.2119 348.6341 0001222 86.1173 273.9959 15.08836364 00
| Epoch (UTC): | 25 May 2026 13:11:51 |
| Eccentricity: | 0.0001222 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 348.6341° |
| argument of perigee: | 86.1173° |
| revolutions per day: | 15.08836364 |
| mean anomaly at epoch: | 273.9959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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