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 66915U 26145.54697374 +.00000000 +00000-0 +46264-4 0 00009
2 66915 50.0045 227.4182 0001103 211.2408 148.8399 13.29322167 00
| Epoch (UTC): | 25 May 2026 13:07:38 |
| Eccentricity: | 0.0001103 |
| inclination: | 50.0045° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.4182° |
| argument of perigee: | 211.2408° |
| revolutions per day: | 13.29322167 |
| mean anomaly at epoch: | 148.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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