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 61070U 26145.55370845 +.00000000 +00000-0 +22109-4 0 00000
2 61070 53.1610 94.2408 0001306 94.4752 265.6398 15.30194023 07
| Epoch (UTC): | 25 May 2026 13:17:20 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 94.2408° |
| argument of perigee: | 94.4752° |
| revolutions per day: | 15.30194023 |
| mean anomaly at epoch: | 265.6398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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