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 03230U 26137.84546463 +.00000000 +00000-0 +12376-3 0 00002
2 03230 74.0288 172.3356 0025329 330.9996 28.9783 15.03653197 03
| Epoch (UTC): | 17 May 2026 20:17:28 |
| Eccentricity: | 0.0025329 |
| inclination: | 74.0288° |
| perigee height: | 538 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 172.3356° |
| argument of perigee: | 330.9996° |
| revolutions per day: | 15.03653197 |
| mean anomaly at epoch: | 28.9783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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