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 53276U 26145.40549714 +.00000000 +00000-0 -62276-3 0 00005
2 53276 53.2138 199.7302 0001017 99.4972 260.6135 15.08892855 01
| Epoch (UTC): | 25 May 2026 09:43:54 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 199.7302° |
| argument of perigee: | 99.4972° |
| revolutions per day: | 15.08892855 |
| mean anomaly at epoch: | 260.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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