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 33320U 26150.50003490 +.00000000 +00000-0 +16044-3 0 00007
2 33320 97.6669 137.0236 0018391 192.1486 167.9288 14.83940607 04
| Epoch (UTC): | 30 May 2026 12:00:03 |
| Eccentricity: | 0.0018391 |
| inclination: | 97.6669° |
| perigee height: | 604 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 137.0236° |
| argument of perigee: | 192.1486° |
| revolutions per day: | 14.83940607 |
| mean anomaly at epoch: | 167.9288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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