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 67287U 26144.48586047 +.00000000 +00000-0 +32379-3 0 00009
2 67287 97.3937 219.7836 0011223 83.7302 276.5214 15.24082799 02
| Epoch (UTC): | 24 May 2026 11:39:38 |
| Eccentricity: | 0.0011223 |
| inclination: | 97.3937° |
| perigee height: | 486 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 219.7836° |
| argument of perigee: | 83.7302° |
| revolutions per day: | 15.24082799 |
| mean anomaly at epoch: | 276.5214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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