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 67394U 26145.24214497 +.00000000 +00000-0 +18960-3 0 00000
2 67394 97.4490 144.6422 0010409 62.7227 297.5066 15.19209410 04
| Epoch (UTC): | 25 May 2026 05:48:41 |
| Eccentricity: | 0.0010409 |
| inclination: | 97.4490° |
| perigee height: | 501 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 144.6422° |
| argument of perigee: | 62.7227° |
| revolutions per day: | 15.19209410 |
| mean anomaly at epoch: | 297.5066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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