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 53316U 26145.54951833 +.00000000 +00000-0 +10207-2 0 00009
2 53316 35.0078 194.2866 0011648 194.5011 165.5389 15.80667709 06
| Epoch (UTC): | 25 May 2026 13:11:18 |
| Eccentricity: | 0.0011648 |
| inclination: | 35.0078° |
| perigee height: | 321 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 194.2866° |
| argument of perigee: | 194.5011° |
| revolutions per day: | 15.80667709 |
| mean anomaly at epoch: | 165.5389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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