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 67401U 26145.27343323 +.00000000 +00000-0 +14919-3 0 00003
2 67401 97.4508 144.6387 0011411 65.1481 295.0939 15.18363338 07
| Epoch (UTC): | 25 May 2026 06:33:44 |
| Eccentricity: | 0.0011411 |
| inclination: | 97.4508° |
| perigee height: | 503 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 144.6387° |
| argument of perigee: | 65.1481° |
| revolutions per day: | 15.18363338 |
| mean anomaly at epoch: | 295.0939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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