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 67115U 26145.54963875 +.00000000 +00000-0 +60352-3 0 00007
2 67115 43.0000 94.6933 0000884 252.6775 107.3980 15.27597254 02
| Epoch (UTC): | 25 May 2026 13:11:28 |
| Eccentricity: | 0.0000884 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.6933° |
| argument of perigee: | 252.6775° |
| revolutions per day: | 15.27597254 |
| mean anomaly at epoch: | 107.3980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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