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 67264U 26144.77911002 +.00000000 +00000-0 +23246-3 0 00002
2 67264 97.4026 219.8613 0016608 92.7925 267.5212 15.22002020 09
| Epoch (UTC): | 24 May 2026 18:41:55 |
| Eccentricity: | 0.0016608 |
| inclination: | 97.4026° |
| perigee height: | 488 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.8613° |
| argument of perigee: | 92.7925° |
| revolutions per day: | 15.22002020 |
| mean anomaly at epoch: | 267.5212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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