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 67676U 26145.60972611 +.00000000 +00000-0 +50760-3 0 00006
2 67676 96.6304 209.7555 0017828 203.0885 156.9556 15.24605082 07
| Epoch (UTC): | 25 May 2026 14:38:00 |
| Eccentricity: | 0.0017828 |
| inclination: | 96.6304° |
| perigee height: | 480 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 209.7555° |
| argument of perigee: | 203.0885° |
| revolutions per day: | 15.24605082 |
| mean anomaly at epoch: | 156.9556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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