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 13777U 26088.09119131 +.00000000 +00000-0 +44135-4 0 00008
2 13777 99.0506 270.4642 0019545 183.3030 176.8008 14.00893002 00
| Epoch (UTC): | 29 March 2026 02:11:18 |
| Eccentricity: | 0.0019545 |
| inclination: | 99.0506° |
| perigee height: | 876 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 270.4642° |
| argument of perigee: | 183.3030° |
| revolutions per day: | 14.00893002 |
| mean anomaly at epoch: | 176.8008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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