▸Orbital parameters

Orbit class	GEO
Inclination	1.2456°
Eccentricity	0.0002630
Period	1436.1 min
Apogee	35,798 km
Perigee	35,776 km
Mean motion	1.00271600 rev/day
RAAN	83.6260°
Arg of perigee	26.7590°
Mean anomaly	74.0242°
B*	0.0000e+0
Rev at epoch	4,676

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 31102U 07009A 26188.05028653 .00000014 00000-0 00000-0 0 9992

2 31102 1.2456 83.6260 0002630 26.7590 74.0242 1.00271600 46761

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ANIK F3",
  "OBJECT_ID": "2007-009A",
  "EPOCH": "2026-07-07T01:12:24.756+00:00",
  "MEAN_MOTION": 1.002716,
  "ECCENTRICITY": 0.000263,
  "INCLINATION": 1.2456,
  "RA_OF_ASC_NODE": 83.626,
  "ARG_OF_PERICENTER": 26.759,
  "MEAN_ANOMALY": 74.0242,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 31102,
  "REV_AT_EPOCH": 4676,
  "BSTAR": 0,
  "MEAN_MOTION_DOT": 1.4e-7,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	ANIK F3
Operator	Telesat CanadaHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	CanadaMEDIUMvia Wikidata
Launch date	Apr 9, 2007HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	4640HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—

▸Data quality

Score90 / 100

Claims8

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/31102

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.