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 25188.16196723 .00000222 00000-0 69316-4 0 9998
2 02802 74.0117 86.5377 0064127 154.0331 206.4069 14.45384993 53541
| Epoch (UTC): | 07 July 2025 03:53:13 |
| Eccentricity: | 0.0064127 |
| inclination: | 74.0117° |
| perigee height: | 695 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 86.5377° |
| argument of perigee: | 154.0331° |
| revolutions per day: | 14.45384993 |
| mean anomaly at epoch: | 206.4069° |
| orbit number at epoch: | 5354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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