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 00029U 26135.22657362 +.00000000 +00000-0 +45402-4 0 00003
2 00029 48.3768 181.2859 0021626 127.9128 232.3745 14.78732954 06
| Epoch (UTC): | 15 May 2026 05:26:15 |
| Eccentricity: | 0.0021626 |
| inclination: | 48.3768° |
| perigee height: | 618 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 181.2859° |
| argument of perigee: | 127.9128° |
| revolutions per day: | 14.78732954 |
| mean anomaly at epoch: | 232.3745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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