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 61670U 26145.54945867 +.00000000 +00000-0 +21572-4 0 00000
2 61670 53.1610 94.0427 0001215 93.6174 266.4965 15.30196393 01
| Epoch (UTC): | 25 May 2026 13:11:13 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.0427° |
| argument of perigee: | 93.6174° |
| revolutions per day: | 15.30196393 |
| mean anomaly at epoch: | 266.4965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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