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 67297U 26145.62027595 +.00000000 +00000-0 +41008-3 0 00004
2 67297 97.3949 221.0354 0009972 82.5958 277.6413 15.24760287 07
| Epoch (UTC): | 25 May 2026 14:53:11 |
| Eccentricity: | 0.0009972 |
| inclination: | 97.3949° |
| perigee height: | 485 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 221.0354° |
| argument of perigee: | 82.5958° |
| revolutions per day: | 15.24760287 |
| mean anomaly at epoch: | 277.6413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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