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 60950U 26145.62996785 +.00000000 +00000-0 +33440-3 0 00000
2 60950 34.9935 339.7564 0000728 253.8807 106.1827 15.23035600 02
| Epoch (UTC): | 25 May 2026 15:07:09 |
| Eccentricity: | 0.0000728 |
| inclination: | 34.9935° |
| perigee height: | 496 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 339.7564° |
| argument of perigee: | 253.8807° |
| revolutions per day: | 15.23035600 |
| mean anomaly at epoch: | 106.1827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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