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 03338U 26088.14749131 +.00000000 +00000-0 +76114-4 0 00007
2 03338 80.6614 148.1234 1130390 104.4125 268.4889 12.23559693 01
| Epoch (UTC): | 29 March 2026 03:32:23 |
| Eccentricity: | 0.1130390 |
| inclination: | 80.6614° |
| perigee height: | 678 km |
| apogee height: | 2476 km |
| right ascension of ascending node: | 148.1234° |
| argument of perigee: | 104.4125° |
| revolutions per day: | 12.23559693 |
| mean anomaly at epoch: | 268.4889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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