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 09984U 26107.47371038 +.00000000 +00000-0 +21192-5 0 00002
2 09984 102.3361 104.0515 0094654 263.8366 253.3899 12.40456946 06
| Epoch (UTC): | 17 April 2026 11:22:08 |
| Eccentricity: | 0.0094654 |
| inclination: | 102.3361° |
| perigee height: | 1430 km |
| apogee height: | 1579 km |
| right ascension of ascending node: | 104.0515° |
| argument of perigee: | 263.8366° |
| revolutions per day: | 12.40456946 |
| mean anomaly at epoch: | 253.3899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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