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 67890U 26145.54264926 +.00000000 +00000-0 +41455-3 0 00001
2 67890 97.2849 79.0276 0001935 91.9065 268.2400 15.33451028 04
| Epoch (UTC): | 25 May 2026 13:01:24 |
| Eccentricity: | 0.0001935 |
| inclination: | 97.2849° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0276° |
| argument of perigee: | 91.9065° |
| revolutions per day: | 15.33451028 |
| mean anomaly at epoch: | 268.2400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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