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 00115U 26131.69133352 +.00000000 +00000-0 +19779-3 0 00001
2 00115 48.1629 280.3900 0025445 94.3729 266.0097 14.98000287 04
| Epoch (UTC): | 11 May 2026 16:35:31 |
| Eccentricity: | 0.0025445 |
| inclination: | 48.1629° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 280.3900° |
| argument of perigee: | 94.3729° |
| revolutions per day: | 14.98000287 |
| mean anomaly at epoch: | 266.0097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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