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 26129.82373132 +.00000000 +00000-0 +21611-3 0 00003
2 00115 48.1630 289.5758 0025487 85.7019 274.6811 14.97991138 02
| Epoch (UTC): | 09 May 2026 19:46:10 |
| Eccentricity: | 0.0025487 |
| inclination: | 48.1630° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 289.5758° |
| argument of perigee: | 85.7019° |
| revolutions per day: | 14.97991138 |
| mean anomaly at epoch: | 274.6811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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