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 04370U 26161.53418390 +.00000000 +00000-0 +92213-4 0 00007
2 04370 74.0392 303.1570 0013509 104.4165 255.8503 14.63391073 04
| Epoch (UTC): | 10 June 2026 12:49:13 |
| Eccentricity: | 0.0013509 |
| inclination: | 74.0392° |
| perigee height: | 673 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 303.1570° |
| argument of perigee: | 104.4165° |
| revolutions per day: | 14.63391073 |
| mean anomaly at epoch: | 255.8503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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