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 48978U 26145.51819316 +.00000000 +00000-0 -42765-3 0 00009
2 48978 87.9099 233.2858 0002316 93.0813 267.0583 13.16594273 09
| Epoch (UTC): | 25 May 2026 12:26:11 |
| Eccentricity: | 0.0002316 |
| inclination: | 87.9099° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2858° |
| argument of perigee: | 93.0813° |
| revolutions per day: | 13.16594273 |
| mean anomaly at epoch: | 267.0583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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