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 00694U 26073.56670005 +.00000000 +00000-0 +27735-3 0 00006
2 00694 30.3517 168.3866 0547623 123.2588 242.1705 14.12087243 07
| Epoch (UTC): | 14 March 2026 13:36:02 |
| Eccentricity: | 0.0547623 |
| inclination: | 30.3517° |
| perigee height: | 456 km |
| apogee height: | 1248 km |
| right ascension of ascending node: | 168.3866° |
| argument of perigee: | 123.2588° |
| revolutions per day: | 14.12087243 |
| mean anomaly at epoch: | 242.1705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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