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 67997U 26145.23250237 +.00000000 +00000-0 +48245-3 0 00009
2 67997 43.0013 336.3131 0001108 283.1097 76.9631 15.27592846 02
| Epoch (UTC): | 25 May 2026 05:34:48 |
| Eccentricity: | 0.0001108 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 336.3131° |
| argument of perigee: | 283.1097° |
| revolutions per day: | 15.27592846 |
| mean anomaly at epoch: | 76.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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