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 67257U 26145.15247807 +.00000000 +00000-0 +37601-3 0 00002
2 67257 97.3937 220.1100 0017070 87.7034 272.6156 15.22618502 08
| Epoch (UTC): | 25 May 2026 03:39:34 |
| Eccentricity: | 0.0017070 |
| inclination: | 97.3937° |
| perigee height: | 486 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 220.1100° |
| argument of perigee: | 87.7034° |
| revolutions per day: | 15.22618502 |
| mean anomaly at epoch: | 272.6156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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