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 21397U 26076.19285641 +.00000000 +00000-0 +15976-3 0 00003
2 21397 82.5199 329.5757 0013201 309.2448 50.7606 15.04860503 09
| Epoch (UTC): | 17 March 2026 04:37:42 |
| Eccentricity: | 0.0013201 |
| inclination: | 82.5199° |
| perigee height: | 543 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 329.5757° |
| argument of perigee: | 309.2448° |
| revolutions per day: | 15.04860503 |
| mean anomaly at epoch: | 50.7606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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