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 07364U 26160.19360500 +.00000000 +00000-0 +42879-4 0 00006
2 07364 81.2318 212.4111 0048354 288.8366 70.7562 14.06460234 09
| Epoch (UTC): | 09 June 2026 04:38:47 |
| Eccentricity: | 0.0048354 |
| inclination: | 81.2318° |
| perigee height: | 836 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 212.4111° |
| argument of perigee: | 288.8366° |
| revolutions per day: | 14.06460234 |
| mean anomaly at epoch: | 70.7562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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