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 16953U 26088.18157823 +.00000000 +00000-0 +11018-3 0 00000
2 16953 74.0096 123.8378 0013287 297.6509 62.3296 14.38827331 01
| Epoch (UTC): | 29 March 2026 04:21:28 |
| Eccentricity: | 0.0013287 |
| inclination: | 74.0096° |
| perigee height: | 753 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 123.8378° |
| argument of perigee: | 297.6509° |
| revolutions per day: | 14.38827331 |
| mean anomaly at epoch: | 62.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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