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 61970U 26145.17527289 +.00000000 +00000-0 +61077-3 0 00009
2 61970 42.9995 108.1960 0001271 269.3951 90.6755 15.27589392 07
| Epoch (UTC): | 25 May 2026 04:12:23 |
| Eccentricity: | 0.0001271 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 108.1960° |
| argument of perigee: | 269.3951° |
| revolutions per day: | 15.27589392 |
| mean anomaly at epoch: | 90.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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