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 42939U 26145.12929550 +.00000000 +00000-0 +00000-0 0 00001
2 42939 64.0769 192.6693 0010318 239.1545 120.8151 2.13101820 05
| Epoch (UTC): | 25 May 2026 03:06:11 |
| Eccentricity: | 0.0010318 |
| inclination: | 64.0769° |
| perigee height: | 19104 km |
| apogee height: | 19156 km |
| right ascension of ascending node: | 192.6693° |
| argument of perigee: | 239.1545° |
| revolutions per day: | 2.13101820 |
| mean anomaly at epoch: | 120.8151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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