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 26131.51018391 +.00000000 +00000-0 +49461-4 0 00003
2 00029 48.3771 198.9470 0021546 111.5126 248.8087 14.78730452 04
| Epoch (UTC): | 11 May 2026 12:14:39 |
| Eccentricity: | 0.0021546 |
| inclination: | 48.3771° |
| perigee height: | 618 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 198.9470° |
| argument of perigee: | 111.5126° |
| revolutions per day: | 14.78730452 |
| mean anomaly at epoch: | 248.8087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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