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 61011U 26145.58514520 +.00000000 +00000-0 +21165-3 0 00008
2 61011 49.9990 187.9120 0002350 167.0005 193.0995 14.84108572 04
| Epoch (UTC): | 25 May 2026 14:02:36 |
| Eccentricity: | 0.0002350 |
| inclination: | 49.9990° |
| perigee height: | 615 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 187.9120° |
| argument of perigee: | 167.0005° |
| revolutions per day: | 14.84108572 |
| mean anomaly at epoch: | 193.0995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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