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 42951U 26145.53420514 +.00000000 +00000-0 +00000-0 0 00006
2 42951 0.0365 349.9972 0004519 67.8608 127.4042 1.00273143 05
| Epoch (UTC): | 25 May 2026 12:49:15 |
| Eccentricity: | 0.0004519 |
| inclination: | 0.0365° |
| perigee height: | 35767 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 349.9972° |
| argument of perigee: | 67.8608° |
| revolutions per day: | 1.00273143 |
| mean anomaly at epoch: | 127.4042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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