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 67370U 26145.24329894 +.00000000 +00000-0 +21995-3 0 00004
2 67370 97.7976 144.1610 0005998 209.1511 150.9372 14.88350632 04
| Epoch (UTC): | 25 May 2026 05:50:21 |
| Eccentricity: | 0.0005998 |
| inclination: | 97.7976° |
| perigee height: | 599 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 144.1610° |
| argument of perigee: | 209.1511° |
| revolutions per day: | 14.88350632 |
| mean anomaly at epoch: | 150.9372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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