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 00694U 63047A 25132.92788820 .00002669 00000-0 31773-3 0 9993
2 00694 30.3571 74.4489 0553723 312.8172 42.7140 14.10553385 89106
| Epoch (UTC): | 12 May 2025 22:16:09 |
| Eccentricity: | 0.0553723 |
| inclination: | 30.3571° |
| perigee height: | 457 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 74.4489° |
| argument of perigee: | 312.8172° |
| revolutions per day: | 14.10553385 |
| mean anomaly at epoch: | 42.7140° |
| orbit number at epoch: | 8910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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