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 67290U 26145.45222970 +.00000000 +00000-0 +38553-3 0 00003
2 67290 97.3939 220.7786 0010832 80.4251 279.8210 15.24402668 09
| Epoch (UTC): | 25 May 2026 10:51:12 |
| Eccentricity: | 0.0010832 |
| inclination: | 97.3939° |
| perigee height: | 485 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 220.7786° |
| argument of perigee: | 80.4251° |
| revolutions per day: | 15.24402668 |
| mean anomaly at epoch: | 279.8210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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