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 13992U 26088.16123758 +.00000000 +00000-0 +99475-4 0 00002
2 13992 74.0510 241.2800 0004518 155.4546 204.6824 14.37563485 00
| Epoch (UTC): | 29 March 2026 03:52:10 |
| Eccentricity: | 0.0004518 |
| inclination: | 74.0510° |
| perigee height: | 763 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 241.2800° |
| argument of perigee: | 155.4546° |
| revolutions per day: | 14.37563485 |
| mean anomaly at epoch: | 204.6824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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