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 61720U 26145.18286631 +.00000000 +00000-0 +10831-3 0 00008
2 61720 53.1602 106.3500 0001479 103.4756 256.6410 15.30193318 05
| Epoch (UTC): | 25 May 2026 04:23:19 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.3500° |
| argument of perigee: | 103.4756° |
| revolutions per day: | 15.30193318 |
| mean anomaly at epoch: | 256.6410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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