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 67961U 26145.48336985 +.00000000 +00000-0 +72125-3 0 00006
2 67961 97.2833 155.4386 0001001 96.4798 263.6559 15.33455823 05
| Epoch (UTC): | 25 May 2026 11:36:03 |
| Eccentricity: | 0.0001001 |
| inclination: | 97.2833° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4386° |
| argument of perigee: | 96.4798° |
| revolutions per day: | 15.33455823 |
| mean anomaly at epoch: | 263.6559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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