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 47502U 26145.06805289 +.00000000 +00000-0 +17579-3 0 00009
2 47502 97.2298 189.8425 0004984 285.6616 74.4077 15.34341960 08
| Epoch (UTC): | 25 May 2026 01:37:59 |
| Eccentricity: | 0.0004984 |
| inclination: | 97.2298° |
| perigee height: | 459 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 189.8425° |
| argument of perigee: | 285.6616° |
| revolutions per day: | 15.34341960 |
| mean anomaly at epoch: | 74.4077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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