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 62656U 26145.15809273 +.00000000 +00000-0 +41826-3 0 00005
2 62656 97.3940 228.2598 0002547 87.9629 272.1904 15.32345875 02
| Epoch (UTC): | 25 May 2026 03:47:39 |
| Eccentricity: | 0.0002547 |
| inclination: | 97.3940° |
| perigee height: | 467 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 228.2598° |
| argument of perigee: | 87.9629° |
| revolutions per day: | 15.32345875 |
| mean anomaly at epoch: | 272.1904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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