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 12998U 26065.56176171 +.00000000 +00000-0 -90877-3 0 00000
2 12998 82.9636 176.4706 0018239 334.7379 35.9826 12.03194329 02
| Epoch (UTC): | 06 March 2026 13:28:56 |
| Eccentricity: | 0.0018239 |
| inclination: | 82.9636° |
| perigee height: | 1652 km |
| apogee height: | 1681 km |
| right ascension of ascending node: | 176.4706° |
| argument of perigee: | 334.7379° |
| revolutions per day: | 12.03194329 |
| mean anomaly at epoch: | 35.9826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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