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 26106.21054692 +.00000000 +00000-0 +16140-3 0 00009
2 00115 48.1636 45.7001 0026629 338.2614 21.7173 14.97854526 08
| Epoch (UTC): | 16 April 2026 05:03:11 |
| Eccentricity: | 0.0026629 |
| inclination: | 48.1636° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 45.7001° |
| argument of perigee: | 338.2614° |
| revolutions per day: | 14.97854526 |
| mean anomaly at epoch: | 21.7173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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