▸Orbital parameters

Orbit class	LEO
Inclination	37.3812°
Eccentricity	0.0003243
Period	92.9 min
Apogee	418 km
Perigee	413 km
Mean motion	15.50416721 rev/day
RAAN	293.2367°
Arg of perigee	71.3707°
Mean anomaly	288.7410°
B*	5.3838e-4
Rev at epoch	10,611

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60454U 24147A 26187.75025859 .00031513 00000-0 53838-3 0 9995

2 60454 37.3812 293.2367 0003243 71.3707 288.7410 15.50416721106115

▸ source OMM (JSON)

{
  "OBJECT_NAME": "EOS-08",
  "OBJECT_ID": "2024-147A",
  "EPOCH": "2026-07-06T18:00:22.342+00:00",
  "MEAN_MOTION": 15.50416721,
  "ECCENTRICITY": 0.0003243,
  "INCLINATION": 37.3812,
  "RA_OF_ASC_NODE": 293.2367,
  "ARG_OF_PERICENTER": 71.3707,
  "MEAN_ANOMALY": 288.741,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60454,
  "REV_AT_EPOCH": 10611,
  "BSTAR": 0.00053838,
  "MEAN_MOTION_DOT": 0.00031513,
  "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	EOS-08
Operator	Indian Space Research OrganizationHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Indian Space Research OrganisationMEDIUMvia Wikidata
Country	IndiaMEDIUMvia Wikidata
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	176HIGH

▸Data quality

Score90 / 100

Claims10

Sources2

TLEavailable

▸Sources

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

▸Actions

GET /api/v1/satellites/60454

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