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 26046.83188378 +.00000000 +00000-0 +35604-3 0 00005
2 00115 48.1639 337.5747 0026606 70.8748 289.5048 14.97319468 08
| Epoch (UTC): | 15 February 2026 19:57:54 |
| Eccentricity: | 0.0026606 |
| inclination: | 48.1639° |
| perigee height: | 557 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 337.5747° |
| argument of perigee: | 70.8748° |
| revolutions per day: | 14.97319468 |
| mean anomaly at epoch: | 289.5048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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