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 28230U 04014A 25189.62475398 .00000537 00000-0 64820-4 0 9992
2 28230 89.8368 56.9680 0003505 88.1498 272.0129 14.82510244601432
| Epoch (UTC): | 08 July 2025 14:59:38 |
| Eccentricity: | 0.0003505 |
| inclination: | 89.8368° |
| perigee height: | 619 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 56.9680° |
| argument of perigee: | 88.1498° |
| revolutions per day: | 14.82510244 |
| mean anomaly at epoch: | 272.0129° |
| orbit number at epoch: | 60143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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