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 57797U 26145.62651719 +.00000000 +00000-0 +81661-4 0 00009
2 57797 98.1958 70.2501 0006388 256.7067 103.3420 14.58703245 02
| Epoch (UTC): | 25 May 2026 15:02:11 |
| Eccentricity: | 0.0006388 |
| inclination: | 98.1958° |
| perigee height: | 693 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 70.2501° |
| argument of perigee: | 256.7067° |
| revolutions per day: | 14.58703245 |
| mean anomaly at epoch: | 103.3420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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