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 61259U 26145.41350183 +.00000000 +00000-0 -44395-5 0 00000
2 61259 53.1602 197.4385 0001006 64.9142 295.1965 15.34389728 09
| Epoch (UTC): | 25 May 2026 09:55:26 |
| Eccentricity: | 0.0001006 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 197.4385° |
| argument of perigee: | 64.9142° |
| revolutions per day: | 15.34389728 |
| mean anomaly at epoch: | 295.1965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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