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 52363U 26145.57156817 +.00000000 +00000-0 +83095-4 0 00009
2 52363 53.2111 213.9873 0000948 88.1293 271.9808 15.08838766 06
| Epoch (UTC): | 25 May 2026 13:43:03 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 213.9873° |
| argument of perigee: | 88.1293° |
| revolutions per day: | 15.08838766 |
| mean anomaly at epoch: | 271.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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