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 52623U 26145.10512200 +.00000000 +00000-0 +69105-4 0 00005
2 52623 53.2160 286.0750 0000300 85.6143 274.4884 15.08841013 03
| Epoch (UTC): | 25 May 2026 02:31:22 |
| Eccentricity: | 0.0000300 |
| inclination: | 53.2160° |
| perigee height: | 540 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 286.0750° |
| argument of perigee: | 85.6143° |
| revolutions per day: | 15.08841013 |
| mean anomaly at epoch: | 274.4884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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