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 26076.18204431 +.00000000 +00000-0 +18646-3 0 00004
2 00694 30.3523 153.7702 0547509 146.3126 217.3543 14.12095533 03
| Epoch (UTC): | 17 March 2026 04:22:08 |
| Eccentricity: | 0.0547509 |
| inclination: | 30.3523° |
| perigee height: | 456 km |
| apogee height: | 1248 km |
| right ascension of ascending node: | 153.7702° |
| argument of perigee: | 146.3126° |
| revolutions per day: | 14.12095533 |
| mean anomaly at epoch: | 217.3543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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