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 67254U 26145.45412287 +.00000000 +00000-0 +35283-3 0 00002
2 67254 97.0846 223.0027 0007083 261.9620 98.0834 15.60736529 06
| Epoch (UTC): | 25 May 2026 10:53:56 |
| Eccentricity: | 0.0007083 |
| inclination: | 97.0846° |
| perigee height: | 381 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 223.0027° |
| argument of perigee: | 261.9620° |
| revolutions per day: | 15.60736529 |
| mean anomaly at epoch: | 98.0834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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