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 67376U 26145.45959227 +.00000000 +00000-0 +73697-4 0 00009
2 67376 97.8037 144.4272 0003142 182.0098 178.1106 14.86342258 04
| Epoch (UTC): | 25 May 2026 11:01:48 |
| Eccentricity: | 0.0003142 |
| inclination: | 97.8037° |
| perigee height: | 607 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 144.4272° |
| argument of perigee: | 182.0098° |
| revolutions per day: | 14.86342258 |
| mean anomaly at epoch: | 178.1106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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