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 02802U 67045B 25188.85410794 .00000194 00000-0 61663-4 0 9996
2 02802 74.0117 85.2456 0064109 152.5571 207.8998 14.45385169 53647
| Epoch (UTC): | 07 July 2025 20:29:54 |
| Eccentricity: | 0.0064109 |
| inclination: | 74.0117° |
| perigee height: | 695 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 85.2456° |
| argument of perigee: | 152.5571° |
| revolutions per day: | 14.45385169 |
| mean anomaly at epoch: | 207.8998° |
| orbit number at epoch: | 5364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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