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 19770U 26074.56854233 +.00000000 +00000-0 +60123-4 0 00008
2 19770 74.0431 280.1303 0005559 283.6458 140.1391 14.40310891 02
| Epoch (UTC): | 15 March 2026 13:38:42 |
| Eccentricity: | 0.0005559 |
| inclination: | 74.0431° |
| perigee height: | 754 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 280.1303° |
| argument of perigee: | 283.6458° |
| revolutions per day: | 14.40310891 |
| mean anomaly at epoch: | 140.1391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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