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 67671U 26145.33742103 +.00000000 +00000-0 +42572-3 0 00004
2 67671 97.2848 178.6607 0000759 101.7439 258.3889 15.33451509 07
| Epoch (UTC): | 25 May 2026 08:05:53 |
| Eccentricity: | 0.0000759 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6607° |
| argument of perigee: | 101.7439° |
| revolutions per day: | 15.33451509 |
| mean anomaly at epoch: | 258.3889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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