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 48340U 26145.60437273 +.00000000 +00000-0 -29285-3 0 00002
2 48340 63.4021 204.3810 0060547 355.1319 4.9111 13.45565846 07
| Epoch (UTC): | 25 May 2026 14:30:17 |
| Eccentricity: | 0.0060547 |
| inclination: | 63.4021° |
| perigee height: | 1043 km |
| apogee height: | 1134 km |
| right ascension of ascending node: | 204.3810° |
| argument of perigee: | 355.1319° |
| revolutions per day: | 13.45565846 |
| mean anomaly at epoch: | 4.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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