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 51142U 26145.39708514 +.00000000 +00000-0 +11348-2 0 00000
2 51142 53.2246 290.7412 0005353 104.5572 255.6021 15.23507145 06
| Epoch (UTC): | 25 May 2026 09:31:48 |
| Eccentricity: | 0.0005353 |
| inclination: | 53.2246° |
| perigee height: | 492 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 290.7412° |
| argument of perigee: | 104.5572° |
| revolutions per day: | 15.23507145 |
| mean anomaly at epoch: | 255.6021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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