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 28353U 26162.08005338 +.00000000 +00000-0 -11638-3 0 00001
2 28353 71.0017 36.5069 0007467 261.8817 98.1458 14.14611092 09
| Epoch (UTC): | 11 June 2026 01:55:16 |
| Eccentricity: | 0.0007467 |
| inclination: | 71.0017° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 36.5069° |
| argument of perigee: | 261.8817° |
| revolutions per day: | 14.14611092 |
| mean anomaly at epoch: | 98.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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