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 26140.96247943 +.00000000 +00000-0 +18293-3 0 00003
2 00115 48.1622 234.7887 0025540 137.1449 223.1466 14.98041133 04
| Epoch (UTC): | 20 May 2026 23:05:58 |
| Eccentricity: | 0.0025540 |
| inclination: | 48.1622° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 234.7887° |
| argument of perigee: | 137.1449° |
| revolutions per day: | 14.98041133 |
| mean anomaly at epoch: | 223.1466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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