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 data is extracted from the following two-line orbital elements,
1 48274U 21035A 25201.07042187 .00009697 00000-0 13548-3 0 9990
2 48274 41.4634 181.2714 0008070 311.2374 48.7767 15.56838821241282
| Epoch (UTC): | 20 July 2025 01:41:24 |
| Eccentricity: | 0.0008070 |
| inclination: | 41.4634° |
| perigee height: | 391 km |
| apogee height: | 402 km |
| right ascension of ascending node: | 181.2714° |
| argument of perigee: | 311.2374° |
| revolutions per day: | 15.56838821 |
| mean anomaly at epoch: | 48.7767° |
| orbit number at epoch: | 24128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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