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 62095U 26144.47351147 +.00000000 +00000-0 +11322-2 0 00005
2 62095 42.9994 306.1279 0001653 274.2078 85.8601 15.70878390 00
| Epoch (UTC): | 24 May 2026 11:21:51 |
| Eccentricity: | 0.0001653 |
| inclination: | 42.9994° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 306.1279° |
| argument of perigee: | 274.2078° |
| revolutions per day: | 15.70878390 |
| mean anomaly at epoch: | 85.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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