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 07369U 26160.42203537 +.00000000 +00000-0 +00000-0 0 00009
2 07369 124.8727 240.7148 0066371 73.1354 281.8900 3.07214579 06
| Epoch (UTC): | 09 June 2026 10:07:43 |
| Eccentricity: | 0.0066371 |
| inclination: | 124.8727° |
| perigee height: | 13477 km |
| apogee height: | 13743 km |
| right ascension of ascending node: | 240.7148° |
| argument of perigee: | 73.1354° |
| revolutions per day: | 3.07214579 |
| mean anomaly at epoch: | 281.8900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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