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 00877U 64053B 25197.64021371 .00000074 00000-0 38976-4 0 9996
2 00877 65.0784 303.1042 0057649 15.9586 344.3312 14.61103910232308
| Epoch (UTC): | 16 July 2025 15:21:54 |
| Eccentricity: | 0.0057649 |
| inclination: | 65.0784° |
| perigee height: | 649 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 303.1042° |
| argument of perigee: | 15.9586° |
| revolutions per day: | 14.61103910 |
| mean anomaly at epoch: | 344.3312° |
| orbit number at epoch: | 23230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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