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 00016U 26101.45278384 +.00000000 +00000-0 +86111-4 0 00002
2 00016 34.2623 137.9993 2019013 198.7510 152.6659 10.49583676 00
| Epoch (UTC): | 11 April 2026 10:52:00 |
| Eccentricity: | 0.2019013 |
| inclination: | 34.2623° |
| perigee height: | 654 km |
| apogee height: | 4213 km |
| right ascension of ascending node: | 137.9993° |
| argument of perigee: | 198.7510° |
| revolutions per day: | 10.49583676 |
| mean anomaly at epoch: | 152.6659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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