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 19970U 26073.47684147 +.00000000 +00000-0 +16196-2 0 00003
2 19970 27.9699 282.2504 5898689 102.2788 326.0412 4.17442610 01
| Epoch (UTC): | 14 March 2026 11:26:39 |
| Eccentricity: | 0.5898689 |
| inclination: | 27.9699° |
| perigee height: | 304 km |
| apogee height: | 19526 km |
| right ascension of ascending node: | 282.2504° |
| argument of perigee: | 102.2788° |
| revolutions per day: | 4.17442610 |
| mean anomaly at epoch: | 326.0412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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