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 26109.14563499 +.00000000 +00000-0 +19799-3 0 00007
2 00115 48.1641 31.2674 0026436 351.6384 8.4091 14.97865079 05
| Epoch (UTC): | 19 April 2026 03:29:42 |
| Eccentricity: | 0.0026436 |
| inclination: | 48.1641° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 31.2674° |
| argument of perigee: | 351.6384° |
| revolutions per day: | 14.97865079 |
| mean anomaly at epoch: | 8.4091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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