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 67284U 26145.16437992 +.00000000 +00000-0 +23048-3 0 00009
2 67284 97.3924 220.2174 0012339 83.1208 277.1432 15.22620330 01
| Epoch (UTC): | 25 May 2026 03:56:42 |
| Eccentricity: | 0.0012339 |
| inclination: | 97.3924° |
| perigee height: | 489 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 220.2174° |
| argument of perigee: | 83.1208° |
| revolutions per day: | 15.22620330 |
| mean anomaly at epoch: | 277.1432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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