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 26047.16553530 +.00000000 +00000-0 +34184-3 0 00000
2 00115 48.1640 335.9356 0026569 72.4438 287.9380 14.97321757 05
| Epoch (UTC): | 16 February 2026 03:58:22 |
| Eccentricity: | 0.0026569 |
| inclination: | 48.1640° |
| perigee height: | 557 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 335.9356° |
| argument of perigee: | 72.4438° |
| revolutions per day: | 14.97321757 |
| mean anomaly at epoch: | 287.9380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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