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 61194U 26145.60168388 +.00000000 +00000-0 +26056-3 0 00004
2 61194 97.5543 235.5141 0017409 43.5494 316.7106 15.08686674 02
| Epoch (UTC): | 25 May 2026 14:26:25 |
| Eccentricity: | 0.0017409 |
| inclination: | 97.5543° |
| perigee height: | 528 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 235.5141° |
| argument of perigee: | 43.5494° |
| revolutions per day: | 15.08686674 |
| mean anomaly at epoch: | 316.7106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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