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 67970U 26145.46160965 +.00000000 +00000-0 +10641-2 0 00001
2 67970 97.2823 155.4673 0001503 101.8695 258.2716 15.33491321 05
| Epoch (UTC): | 25 May 2026 11:04:43 |
| Eccentricity: | 0.0001503 |
| inclination: | 97.2823° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4673° |
| argument of perigee: | 101.8695° |
| revolutions per day: | 15.33491321 |
| mean anomaly at epoch: | 258.2716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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