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 06153U 26106.64193005 +.00000000 +00000-0 +37333-4 0 00004
2 06153 35.0055 81.0768 0006078 113.9543 52.5808 14.60026357 04
| Epoch (UTC): | 16 April 2026 15:24:22 |
| Eccentricity: | 0.0006078 |
| inclination: | 35.0055° |
| perigee height: | 689 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 81.0768° |
| argument of perigee: | 113.9543° |
| revolutions per day: | 14.60026357 |
| mean anomaly at epoch: | 52.5808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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