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 28650U 26106.86989811 +.00000000 +00000-0 +20825-3 0 00009
2 28650 97.9953 127.3536 0018142 242.1552 117.7838 15.09189729 05
| Epoch (UTC): | 16 April 2026 20:52:39 |
| Eccentricity: | 0.0018142 |
| inclination: | 97.9953° |
| perigee height: | 526 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 127.3536° |
| argument of perigee: | 242.1552° |
| revolutions per day: | 15.09189729 |
| mean anomaly at epoch: | 117.7838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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