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 12997U 26154.29535795 +.00000000 +00000-0 +37593-3 0 00004
2 12997 82.9593 271.9641 0057247 294.6564 123.4901 12.15871439 08
| Epoch (UTC): | 03 June 2026 07:05:18 |
| Eccentricity: | 0.0057247 |
| inclination: | 82.9593° |
| perigee height: | 1565 km |
| apogee height: | 1656 km |
| right ascension of ascending node: | 271.9641° |
| argument of perigee: | 294.6564° |
| revolutions per day: | 12.15871439 |
| mean anomaly at epoch: | 123.4901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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