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 26039.29118977 +.00000000 +00000-0 +35147-3 0 00007
2 00115 48.1637 14.6211 0026842 36.1231 324.1494 14.97259038 06
| Epoch (UTC): | 08 February 2026 06:59:18 |
| Eccentricity: | 0.0026842 |
| inclination: | 48.1637° |
| perigee height: | 557 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 14.6211° |
| argument of perigee: | 36.1231° |
| revolutions per day: | 14.97259038 |
| mean anomaly at epoch: | 324.1494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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